G-6_Launch_Vehicle_Data_Collection_Requirements_Template_-_28_Oct_15.xlsx
XLSX spreadsheet 2 MB Posted
- Attached to
- AFCAA Cost Estimating Modeling (CEM) Support Federal contract opportunity
- Solicitation number
- FA7014-16-R-5004
About this file
G-6 Launch Vehicle Data Collection Requirements Template (DRAFT) 28 Oct 15
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Text version
Program
| ProgramTemplate | UNCLASSIFIED, FOR OFFICIAL USE ONLY | TagName1 | TagValue1 |
| AFCAA CEM Templates | TagName2 | TagValue2 | |
| Program Template | TagName3 | TagValue3 |
| ColumnHead | Parameter Name | Value | Unit of Measure | Estimate or Actual | Source | Notes | Definition of Parameter | VocabularyID |
| Program Name | Program Name | DCARCMetadata | ||||||
| Program Name | DCARC defined Program Name | DCARCMetadata | ||||||
| Name - Short | DCARC defined, acronym | CEMVocab | ||||||
| Name - Popular | An optional alternative name | CEMVocab | ||||||
| Program Description | DCARC defined program description | CEMVocab | ||||||
| Program Number | Program Number | DCARCMetadata | ||||||
| Mil-Handbook | Mil-STD-881 Appendix | DCARCMetadata | ||||||
| Weapon System Type | DCARC defined | DCARCMetadata | ||||||
| Lead Service | DCARC defined Service/Component | DCARCMetadata | ||||||
| Other Services | If a program is "Joint", then list other services involved in the program. | DCARCMetadata | ||||||
| Procuring Organization | SysCom | DCARCMetadata | ||||||
| Program Office | PEO or Program Office | DCARCMetadata | ||||||
| Initial Selected Acquisition Review (SAR) | Date from DAMIR | DCARCMetadata | ||||||
| Latest Selected Acquisition Review (SAR) | Date from DAMIR | DCARCMetadata | ||||||
| Upgrade/Modernization | Yes/No category | CEMVocab | ||||||
| Subprogram Name | Subprogram name if applicable | CEMVocab | ||||||
| Model | Specific configuration or designated model number | CEMVocab |
UOM is N/A for this sheet. Column included only for shape consistency.
Est/Act is N/A for this sheet. Column included only for shape consistency.
Enter text for each parameter.
Milestone
| MilestoneTable | UNCLASSIFIED, FOR OFFICIAL USE ONLY | TagName1 | TagValue1 |
| AFCAA CEM Templates | TagName2 | TagValue2 | |
| Milestone Template | TagName3 | TagValue3 |
| ColumnHead | Subprogram Name | |||||||||||||
| Parameter Name | Subprogram | Value | Units | Estimate or Actual | Source | Notes | Value | Units | Estimate or Actual | Source | Notes | Definition of Parameter | VocabularyID | |
| Material Development Decision | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Completion Date | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Milestone A | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Contract Award | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Capability Development Document (CDD) Validation | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Development RFP Release Decision | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Risk Reduction Build | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Milestone B | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| EMD Contract Award | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| System Requirements Review (SRR) | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Preliminary Design Review (PDR) | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Critical Design Review (CDR) | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| First Delivery | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| First Flight | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Development Test & Evaluation Begin | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Development Test & Evaluation End | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Operational Test & Evaluation Begin | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Operational Test & Evaluation End | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Limited Deployment Decision | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Integration Build | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Milestone C | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Limited Deployment | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Full Deployment Decision (FDD) | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Low Rate Initial Production Contract Award | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Full Rate Production (FRP) Decision | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Full Rate Production Contract Award | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Initial Operational Capability (IOC) | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Full Deployment (FD) | Date | DDMMMYY | Milestone Date | CEMVocab | ||||||||||
| Full Operational Capability (FOC) | Date | DDMMMYY | Milestone Date | CEMVocab |
Enter parameter values as a single date value in this column.
Identify if the parameter value is an actual value or an estimated value.
Enter parameter values as a single date value in this column.
Identify if the parameter value is an actual value (A) or an estimated value (E).
If these columns are expanded and used to convey a second subprogram or model, take care to each case in the first column heading cell.
When any parameter calls for additional detail, insert rows underneath and indent sub-names as needed.
For additional columns to express alternative designs, hit Ungroup button above.
When parameter varies by subprogram, enter subprogram name in this column.
If no subprograms, then leave this column empty.
Acquisition (CEM)
| AcquisitionTemplate | UNCLASSIFIED, FOR OFFICIAL USE ONLY | TagName1 | TagValue1 |
| AFCAA CEM Templates | TagName2 | TagValue2 | |
| Acquisition Template | TagName3 | TagValue3 |
| Material Solution Analysis | Technology Maturation and Risk Reduction | Engineering and Manufacturing Development | Production and Deployment | Sustainment | Disposal | ||||||||||||||||||
| LRIP 1 | LRIP 2 | FRP 1 | FRP 2 | ||||||||||||||||||||
| Contract A | Contract B | Contract A | Contract B | Contract A | Contract B | Contract (Prime) | Contract (Sub) | Contract (Prime) | Contract (Sub) | Contract (Prime) | Contract (Sub) | Contract (Prime) | Contract (Sub) |
| ColumnHead | Parameter name | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Value | Unit of Measure | Units Qualifier | Definition of Parameter | VocabularyID |
| Name - Phase/Contract/Lot | Name/Number | The common name of this phase, contract, or lot. | CEMVocab | ||||||||||||||||||||||||||
| Subphase Name | Name/Number | The common name of this subphase. | CEMVocab | ||||||||||||||||||||||||||
| Contract Number | Name/Number | Prime contract number | CEMVocab | ||||||||||||||||||||||||||
| Option Number | Name/Number | Contract option number if applicable | CEMVocab | ||||||||||||||||||||||||||
| Subcontract Number | Name/Number | Subcontract number. | CEMVocab | ||||||||||||||||||||||||||
| Model | Name/Number | Specific configuration or designated model number | CEMVocab | ||||||||||||||||||||||||||
| Quantity | Quantity | The number of units produced for this Phase | CEMVocab | ||||||||||||||||||||||||||
| Quantity | Quantity | Units for the quantity cited above (e.g. Aircraft, Missiles, Pods, Kits, etc.) | CEMVocab | ||||||||||||||||||||||||||
| Award Date | Date | Date of contract award announcement or beginning of phase. | CEMVocab | ||||||||||||||||||||||||||
| First Delivery Date | Date | The date of the first delivery. | CEMVocab | ||||||||||||||||||||||||||
| End Date | Date | The end data of this phase, contract, or lot. | CEMVocab | ||||||||||||||||||||||||||
| Contracting Strategy | Description | by Phase | Describe this phase's contracting strategy. | CEMVocab | |||||||||||||||||||||||||
| Competition Approach | List | List the Competition Approach: None; Full Phase Competed; Competition thru CDR; etc. | CEMVocab | ||||||||||||||||||||||||||
| Warranty | List | Is there a warranty for this lot? | CEMVocab | ||||||||||||||||||||||||||
| Warranty Type | Description | Describe Warranty | CEMVocab | ||||||||||||||||||||||||||
| Capital Investment | List | Is this the first lot to benefit from capital investment, tooling, plant rearrangement, etc.? | CEMVocab | ||||||||||||||||||||||||||
| Capital Investment Description | Description | Describe capital improvements. | CEMVocab | ||||||||||||||||||||||||||
| Government Test Agency | Name/Number | List Agencies and MIPR or WR numbers | CEMVocab | ||||||||||||||||||||||||||
| Production Rate - Planned Minimum Sustaining | Quantity | Minimum | Minimum economic rate of production. | CEMVocab | |||||||||||||||||||||||||
| Production Rate - Planned 1-8-5 | Quantity | Planned 1-8-5 | Rate of production with factory operating at a single shift. | CEMVocab | |||||||||||||||||||||||||
| Production Rate - Planned Maximum | Quantity | Maximum | Maximum production rate without shift constraints. | CEMVocab | |||||||||||||||||||||||||
| Contractor Name | Name/Number | Name of contractor | CEMVocab | ||||||||||||||||||||||||||
| Special Cases | Description | Define. | CEMVocab | ||||||||||||||||||||||||||
| Additional Information - Program Level | Description | Program Level | Define. | CEMVocab | |||||||||||||||||||||||||
| Funding Appropriation | List | Appropriation code | CEMVocab | ||||||||||||||||||||||||||
| Funding Year | Year | Purpose to track to Budget Exhibits (e.g. capture GFE cost) | CEMVocab | ||||||||||||||||||||||||||
| Multiyear Production | List | Is this lot part of a multiyear contract? | CEMVocab | ||||||||||||||||||||||||||
| Concurrent Production | List | Are there other customers during this phase/lot such as Foreign Military Sales? | CEMVocab | ||||||||||||||||||||||||||
| Information Assurance | Description | List amount of information assurance required. | CEMVocab | ||||||||||||||||||||||||||
| Launch Vehicle Type | List | What type(s) and variant(s) of Launch Vehicle(s) will the Space Vehicle be launched on? | CEMVocab | ||||||||||||||||||||||||||
| Scope of contract | Description | Define. | CEMVocab | ||||||||||||||||||||||||||
| GFE payloads | Description | ??? | Is the Space Vehicle hosting any other payloads for other missions? List and provide description.M44 | CEMVocab | |||||||||||||||||||||||||
| Contract Type | List | What contract type(s) are associated with the program? (Ex: CPFF, CPIF, CPAF, FPIF, FFP, T&M, etc) | CEMVocab | ||||||||||||||||||||||||||
| System Integration Contract | List | Is the system integration effort on this contract? | CEMVocab | ||||||||||||||||||||||||||
| Fee Structure Type | List | What Fee/Incentive structure is associated with the contract(s)? (Ex: Incentive Fee, Award Fee, Performance Fee, Fixed Fee, Milestone Payments, etc) | CEMVocab | ||||||||||||||||||||||||||
| Government Provided Facility | List | List of available facilities where vehicle can be processed and launched | CEMVocab |
The column headings shown are an example only. Modify headings and insert additional columns as needed to fully describe the acquisition plan.
Describe each Phase, Contract, and/or Lot.
Consider using a time-phased Table to fully describe annual quantities. See adjacent sheet "Quantities and O&S Time Phased" Copy the Model and Quantity rows and repeat for each Model or Configured End Item as needed
Quantities and O&S Time Phase
| TimePhasedTableQuantity | UNCLASSIFIED, FOR OFFICIAL USE ONLY | TagName1 | TagValue1 |
| AFCAA CEM Templates | TagName2 | TagValue2 | |
| Acquisition Quantities, Fielding, and O&S Time Phased Template | TagName3 | TagValue3 |
| ColumnHead | Item Name | YR 1 | YR 2 | YR 3 | YR 4 | YR 5 | YR 6 | YR 7 | YR 8 | YR 9 | YR 10 | YR n … | Long Lead Requirements | Unit of Measure | Unit Qualifier | Source | Notes | Definition of Parameter | VocabularyID |
| Designate each column as Estimate or Actual ---> |
| Quantity - Prototype | Quantity | Prototype Systems | Prototypes delivered per year. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Quantity - Procurement | Quantity | Systems | Equipment procured by year funded. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Quantity - Concurrent Production | Quantity | Systems | Concurrent production represents units produced by the contractor for other parties such as Foreign Military Sales or any other customer. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Number of Deliveries | Quantity | Systems | Equipment delivered by year delivered or installations by year installed | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Launch Schedule - Actual | Quantity | by Year | CEMVocab |
| End Item #1 | |||
| End Item #2 | |||
| End Item #3 | |||
| End Item #4 | |||
| … | |||
| Training Item #1 | |||
| Training Item #2 | |||
| … | |||
| Support Equipment Item #1 | |||
| Support Equipment Item #2 | |||
| … |
| Inventory or Fielded Density | Quantity | Systems | Total number of systems supported by year. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Inventory or Fielded Density | Quantity | Systems | Total number of systems supported by year. | CEMVocab |
| Squadron #1/Base #1 | ||||
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … | ||||
| Squadron #2/Base #2 | ||||
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … | ||||
| Squadron #3/Base #3 | ||||
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … | ||||
| Operational Activity | Hours, Miles, Sorties | System usage expressed as hours or miles per system per year by various operational states. | CEMVocab | |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Operational Activity |
| System Use (OPTEMPO), miles driven |
| Location #1 or Operational State #1 |
| End Item #1 |
| End Item #2 |
| End Item #3 |
| End Item #4 |
| … |
| System Use (OPTEMPO), hours operated |
| Location #1 or Operational State #1 |
| End Item #1 |
| End Item #2 |
| End Item #3 |
| End Item #4 |
| … |
| Number of Caps/Sorties |
| Number of Users |
| Number of Concurrent Users |
| System Throughput (Transactions) |
| Data Storgage |
| Number of Disposals | Quantity | Systems | Annual quantity of items leaving service at end of useful life. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Number of Overhauls or Scheduled Depot Maintenance | Quantity | Systems | The planned number of depot scheduled events by year. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Number of Hardware Modification Kit Procurement | Quantity | Kits | The planned number of kits procured by year to support hardware modification events. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Number of Hardware Modification Installs | Quantity | Installs | The planned number of hardware modification events by year. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … |
| Number of NDI Refresh Events | Quantity | Refreshes | The number of Information Systems related refreshes (number of hardware items procured and installed) per year. | CEMVocab |
| End Item #1 | ||||
| End Item #2 | ||||
| End Item #3 | ||||
| End Item #4 | ||||
| … | ||||
| Training Item #1 | ||||
| Training Item #2 | ||||
| … | ||||
| Support Equipment Item #1 | ||||
| Support Equipment Item #2 | ||||
| … | ||||
| Number of Training Events | Quantity | Classes | The number of training events per class per year. | CEMVocab |
| Class #1 | ||||
| Class #2 | ||||
| Class #3 | ||||
| Class #4 |
| Number of Base Activation | Quantity | Bases | The number of sites activated per year. | CEMVocab |
| Test Squadron | ||||
| Operator Training | ||||
| Maintainer Training | ||||
| Squadron #1/Base #1 | ||||
| Squadron #2/Base #2 | ||||
| Squadron #3/Base #3 | ||||
| Squadron #4/Base #4 | ||||
| … |
Enter name of item.
Use headings in bold and indent wherever it is useful to do so.
All entries below are examples only.
Enter annual values here.
Note early years may be know and future years forecasted. Designate in row 6.
For procurement quantities, enter text describing long-lead requirements. Could be expressed as a percent of funds or names of specific items that must be purchased early.
Otherwise leave blank.
Unit of Measure is Aircraft, Engines, AURs, Radars, Silos, Sites, etc.
Enter annual quantities here. For prototypes convey the year delivered.
Include non-PME as well as PME.
Enter annual quantity installed or delivered here.
This is pertinent for modeling fielding event costs.
Enter the cumulative quantities delivered and supported here.
This is pertinent for modeling O&S costs.
Show ramp-down of items leaving service at end of useful life.
Enter quantity of sites activated here.
Entries often will simply be 1 if each site is explicitly named in column C..
This is pertinent for modeling base activation costs and to begin O&S of location costs.
Enter annual quantity of kits purchased for modification events here.
This is pertinent for modeling Mods costs.
Enter annual quantity of items leaving service at end of useful life.
This is pertinent for modeling disposal costs as well as density ramp-down.
Begin at earliest year quantity data is applicable.
List all program years. Avoid using Prior and To-complete columns - be explicit.
Enter the cumulative quantities delivered and supported by location here.
This is pertinent for modeling O&S costs.
Show ramp-down of items leaving service at end of useful life.
Enter annual quantities here. For procurement convey the year funded.
Include non-PME as well as PME.
Enter annual quantity of overhauls or any other scheduled Depot activity here.
This is pertinent for modeling Depot costs.
Enter annual quantity of NDA refresh events here.
This is pertinent for modeling refresh cycle costs.
Other potential usage measures. Enter annual activity. Expand by Location or End Item as needed.
Enter annual quantity of modification installs here.
This is pertinent for modeling Mods costs.
Enter annual concurrent production quantities here. Concurrent production represents units produced by the contractor for other parties such as Foreign Military Sales or any other customer.
For each Operational Activity row, expand by Location or or operational state. Then further expand by End Item/Variant as needed. Enter annual activity in columns.
Roles
| RolesTable | UNCLASSIFIED, FOR OFFICIAL USE ONLY | TagName1 | TagValue1 |
| AFCAA CEM Templates | TagName2 | TagValue2 | |
| Roles Template | TagName3 | TagValue3 |
| ColumnHead | WBS/CRS Number | WBS/CRS Element | Government Role | Prime Contractor | Secondary Subcontractor/Supplier/Third Party | Tertiary Subcontractor/Supplier/Third Party | Notes |
| 1.0 | Launch Vehicle System | ||||||
| 1.1 | System Engineering, Integration, Test, Program Management (SEIT/PM) | ||||||
| 1.1.1 | System Engineering (SE) | ||||||
| 1.1.2 | Integration and Test | ||||||
| 1.1.3 | Program Management | ||||||
| 1.1.4 | Factory Support | ||||||
| 1.1.5 | Special Studies | ||||||
| 1.1.6 | Data | ||||||
| 1.1.6.1 | Technical Publications | ||||||
| 1.1.6.2 | Engineering Data | ||||||
| 1.1.6.3 | Management Data | ||||||
| 1.1.6.4 | Support Data | ||||||
| 1.1.6.5 | Data Depository | ||||||
| 1.1.7 | Peculiar Support Equipment | ||||||
| 1.1.7.1 | Test and Measurement Equipment | ||||||
| 1.1.7.2 | Support and Handling Equipment | ||||||
| 1.1.8 | Common Support Equipment | ||||||
| 1.1.8.1 | Test and Measurement Equipment | ||||||
| 1.1.8.2 | Support and Handling Equipment | ||||||
| 1.2 | Launch Vehicle | ||||||
| 1.2.1 | SEIT/PM | ||||||
| 1.2.1.1 | System Engineering | ||||||
| 1.2.1.2 | Integration, Assembly, Test & Checkout (IAT&C) | ||||||
| 1.2.1.3 | Program Management | ||||||
| 1.2.2 | Stages 1…n (Specify) | ||||||
| 1.2.2.1 | SEIT/PM | ||||||
| 1.2.2.1.1 | System Engineering (SE) | ||||||
| 1.2.2.1.2 | Integration and Test | ||||||
| 1.2.2.1.3 | Program Management | ||||||
| 1.2.2.2 | Structures and Mechanisms | ||||||
| 1.2.2.2.1 | Structures (Booster or Upper Stages) | ||||||
| 1.2.2.2.2 | Interstage Adapters, Stub Adapters, Forward Adapters | ||||||
| 1.2.2.2.3 | Aft Transition Structure | ||||||
| 1.2.2.2.4 | Heat Shield | ||||||
| 1.2.2.2.5 | Mechanisms | ||||||
| 1.2.2.3 | Propulsions System | ||||||
| 1.2.2.3.1 | Liquid Engines | ||||||
| 1.2.2.3.2 | Solid Rocket Motors | ||||||
| 1.2.2.3.3 | Propulsion Feed Systems | ||||||
| 1.2.2.4 | Mission Assurance Instrumentation | ||||||
| 1.2.2.5 | Reaction Control System | ||||||
| 1.2.2.6 | Recovery System | ||||||
| 1.2.2.7 | Environmental Control System | ||||||
| 1.2.2.8 | Guidance navigation and Control | ||||||
| 1.2.2.9 | Power | ||||||
| 1.2.2.10 | Data Acquisition and Telemetry | ||||||
| 1.2.2.11 | Range Tracking & Safety (Airborne) | ||||||
| 1.2.2.12 | Flight Software Release 1…n | ||||||
| 1.2.2.13 | Electrical Cabling, Connectors, and Transducers | ||||||
| 1.2.2.14 | Other Stage Systems 1…n (Specify) | ||||||
| 1.2.3 | Payload Accommodations 1…n (Specify) | ||||||
| 1.2.3.1 | SEIT/PM | ||||||
| 1.2.3.2 | Payload Fairing | ||||||
| 1.2.3.3 | Payload Attach Fitting (Adapter) | ||||||
| 1.2.3.4 | Mission Unique Hardware (Launch vehicle) 1…n (Specify) | ||||||
| 1.2.4 | Other Launch Vehicle Systems 1…n (Specify) | ||||||
| 1.3 | Mission Integration and Analysis 1…f (Specify) | ||||||
| 1.3.1 | Mission Standard Integration & Analysis | ||||||
| 1.3.2 | Mission Unique Integration & Analysis 1...n (Specify) | ||||||
| 1.3.3 | Mission Unique Development/Design | ||||||
| 1.3.4 | Mission Assurance | ||||||
| 1.4 | Launch Operations Site | ||||||
| 1.4.1 | SEIT/PM | ||||||
| 1.4.2 | Vehicle Processing and Checkout | ||||||
| 1.4.3 | Mission Services | ||||||
| 1.4.3.1 | Mission Unique Hardware (Launch Operations) 1…n (Specify) | ||||||
| 1.4.3.2 | Space Vehicle Processing | ||||||
| 1.4.3.3 | Transportation | ||||||
| 1.4.4 | Launch | ||||||
| 1.4.5 | Flight Operations | ||||||
| 1.4.6 | Post Launch | ||||||
| 1.4.6.1 | Recovery Operations and Services | ||||||
| 1.4.6.2 | Post Launch Refurbishment | ||||||
| 1.4.7 | Site Maintenance | ||||||
| 1.4.8 | Base Support | ||||||
| 1.4.9 | Range Tracking & Safety (Ground) | ||||||
| 1.4.9.1 | Range Ground System | ||||||
| 1.4.9.2 | Range Operations | ||||||
| 1.4.10 | Launch Propellants | ||||||
| 1.5 | Launch Site 1…n (Specify) | ||||||
| 1.5.1 | SEIT/PM | ||||||
| 1.5.2 | Operational/Site Activation | ||||||
| 1.5.3 | Peculiar Support Equipment | ||||||
| 1.5.4 | Ground Command, Control and Communications (GC3) | ||||||
| 1.5.4.1 | SEIT/PM | ||||||
| 1.5.4.2 | Command, Control and Communication | ||||||
| 1.5.4.3 | Other Ground 1…n (Specify) | ||||||
| 1.6 | System Test and Evaluation | ||||||
| 1.6.1 | Development Test and Evaluation | ||||||
| 1.6.2 | Operational Test and Evaluation | ||||||
| 1.6.3 | Mock-ups/System Integration labs (SILs) | ||||||
| 1.6.4 | Test and Evaluation Support | ||||||
| 1.6.5 | Test Facilities | ||||||
| 1.7 | Industrial Facilities | ||||||
| 1.7.1 | Construction/Conversion/Expansion | ||||||
| 1.7.2 | Equipment Acquisition or Modernization | ||||||
| 1.7.3 | Maintenance (Industrial Facilities) | ||||||
| 1.8 | Initial Spares and Repair Parts |
Specify Government's Role by WBS Element (e.g. GFE, Test, Depot Activation).
Specify Prime Contractor Name by WBS Element.
Specify Subcontractor/Supplier/3rd Party by name. Elaborate on specific role or contracting arrangement in Notes if needed.
HW Tech Table
| HardwareTechnicalDetailTable | UNCLASSIFIED, FOR OFFICIAL USE ONLY | TagName1 | TagValue1 | ||||||||||||||||||||||||||||||||||||||||||||||
| CARD | TagName2 | TagValue2 | |||||||||||||||||||||||||||||||||||||||||||||||
| PMP Hardware Technical Table, Aircraft, Engine | TagName3 | TagValue3 | |||||||||||||||||||||||||||||||||||||||||||||||
| ColumnHead | Second Reference Design (e.g. Contractor A) | Third Reference Design (e.g. Contractor B) | Time each parameter is expected to be available | ||||||||||||||||||||||||||||||||||||||||||||||
| WBS/CRS Number | WBS/CRS Element | Parameter Name | Value | Low | High | Margin | Unit of Measure | Unit Qualifier | Estimate or Actual | Objective | Threshold | Source | Notes | Value | Low | High | Margin | Unit of Measure | Unit Qualifier | Estimate or Actual | Source | Notes | Value | Low | High | Margin | Unit of Measure | Unit Qualifier | Estimate or Actual | Source | Notes | Definition | VocabularyID | List Item 1 | List Item 2 | List Item 3 | List Item 4 | List Item 5 | List Item 6 | List Item 7 | List Item 8 | List Item 9 | List Item 10 | List Item n=… | MS A | PDR | MS B | CDR | |
| 1.0 | Launch Vehicle System | ||||||||||||||||||||||||||||||||||||||||||||||||
| 1.2 | Launch Vehicle | ||||||||||||||||||||||||||||||||||||||||||||||||
| Length Overall | ft | x | |||||||||||||||||||||||||||||||||||||||||||||||
| Total Weight (Including Propellants) | lb | Physical weight (use at least 1 decimal place). | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Propellant Weight ( All Propellants) | lb | Physical weight (use at least 1 decimal place). | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Number of Stages | # | Number of Stages | x | x | x | x | |||||||||||||||||||||||||||||||||||||||||||
| Man-Rated | Y/N | Is element man-rated? | x | x | x | x | |||||||||||||||||||||||||||||||||||||||||||
| Reusable Subsystems (list) | Look up | x | |||||||||||||||||||||||||||||||||||||||||||||||
| Performance to Various Orbits (Launch Vehicles) | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Number of flights to date | Count | Number of flights to date | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Number of succesful flights | Count | Number of succesful flights | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Number of flight failures due to motor | Count | Number of flight failures due to motor | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Launch Locks | Launch lock count | x | |||||||||||||||||||||||||||||||||||||||||||||||
| Weight LV Margin | Launch Mass Margin percent | x | |||||||||||||||||||||||||||||||||||||||||||||||
| Restock due to obsolescence | x | x | |||||||||||||||||||||||||||||||||||||||||||||||
| Shelf Life | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Reliability | Space Vehicle Level | x | x | x | |||||||||||||||||||||||||||||||||||||||||||||
| 1.2.2 | Stages 1…n (Specify) | ||||||||||||||||||||||||||||||||||||||||||||||||
| Stage Diameter | ft | Physical measurement. | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Stage Length | ft | Physical measurement (use at least 1 decimal place). | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Stage Weight, Empty | lbs | Physical weight (use at least 1 decimal place). | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Stage Propellant Capacity | lbs | x | |||||||||||||||||||||||||||||||||||||||||||||||
| Type of Corration Control | Text | x | |||||||||||||||||||||||||||||||||||||||||||||||
| New Design | Percentage | x | x | x | |||||||||||||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | ||||||||||||||||||||||||||||||||||||||||||||
| 1.2.2.2 | Structures and Mechanisms | ||||||||||||||||||||||||||||||||||||||||||||||||
| Number of Structural Subassemblies | Count | Number of Structural Subassemblies | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Primary Structural Material | Text | Materials used in the construction of the item. | x | x | x | x | |||||||||||||||||||||||||||||||||||||||||||
| Ignition mechanism | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Nozzle extension cone | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Nozzle throat | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Motor case | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Igniter body | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Body of safe-arm device | x | ||||||||||||||||||||||||||||||||||||||||||||||||
| Insulator material | x | x | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Inhibitor material | x | x | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Number of Articulations | # | Number of Articulations | x | ||||||||||||||||||||||||||||||||||||||||||||||
| New Design | Percentage | x | x | x | |||||||||||||||||||||||||||||||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | |||||||||||||||||||||||||||||||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | ||||||||||||||||||||||||||||||||||||||||||||
| 1.2.2.2.1 | Structures (Booster or Upper Stages) | ||||||||||||||||||||||||||||||||||||||||||||||||
| Weight of Structure | lbs | Physical weight (use at least 1 decimal place). | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Volume of Structure | cu in | Physical measured size of the item. | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Primary Structural Material | Text | Materials used in the construction of the item. | x | x | x | x | |||||||||||||||||||||||||||||||||||||||||||
| Number of Interfaces | # | Number of Interfaces | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Aerodynamic | Y/N | Is element aerodynamic? | x | ||||||||||||||||||||||||||||||||||||||||||||||
| Ignition mechanism |
akkilcullen: akkilcullen:
why is this parameter listed on the liquid engines and not solid engines?
Do solid engines not have ignitions.
| Placed at the structure level so be safe. | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Nozzle extension cone | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Nozzle throat | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Motor case | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Igniter body | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Body of safe-arm device | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Insulator material | x | x | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Inhibitor material | x | x | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of ignition squibs | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Required voltage for ignition squibs | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Required current for ignition squibs | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Safe-arm device actuation | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Power requirement for safe-arm device | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Number of Articulations | # | Number of Articulations | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.2.3 | Aft Transition Structure | ||||||||||||||||||||||||
| Number of Articulations | # | Number of Articulations | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.2.4 | Heat Shield | ||||||||||||||||||||||||
| Maximum temperature | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Minimum temperature | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.3 | Propulsions System | ||||||||||||||||||||||||
| Type (cryogenic/semi-cryogenic/storable/hypergolic) | x | x | Contractor | 1 | 1 | ||||||||||||||||||||
| Oxidiser | x | x | Contractor | 1 | 1 | ||||||||||||||||||||
| Fuel | x | x | Contractor | 1 | 1 | ||||||||||||||||||||
| Oxidiser density | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Fuel density | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Oxidiser-to-fuel ratio (O/F) | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Oxidixer + mass% | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Binder material + mass% | x | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Additives + mass% | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Propellant density | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Pressurization | psi | Maximum operating pressure in psi (pound per square inch or, more accurately, pound-force per square inch) | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of Coolant Passages | # | Number of Coolant Passages | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Number of Pump Stages | # | Number of Pump Stages | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.3.1 | Liquid Engines | ||||||||||||||||||||||||
| Number of Engines per Vehicle (values below are per engine) | # | Number of Engines per Vehicle (values below are per engine) | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| First Production Year | Year | First Production Year | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Man-Rated | Y/N | Is element man-rated? | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Specific impulse - Vacuum | Vacuum | x | x | Contractor | 1 | 1 | |||||||||||||||||||
| Specific impulse - Sea level | Sea level | x | x | Contractor | 1 | 1 | |||||||||||||||||||
| Maximum thrust - Vacuum | Vacuum | Maximum thrust (vacuum/sea level) | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Maximum firing time | Maximum firing time | x | x | Contractor | 1 | 1 | |||||||||||||||||||
| Average chamber pressure | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Maximum chamber pressure | Maximum chamber pressure | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Operating oxidizer/fuel ratio | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Combustion chamber oxidizer/fuel ratio | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Maximum allowable spin speed | Maximum allowable spin speed | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Thrust misalignment from motor axis | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Thrust of-set from motor axis | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Degree of TMC | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Degree of TVC | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Maximum number of consecutive firings | Maximum number of consecutive firings | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Minimum impulse bit | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Maximum thrust - Sea level | Sea level | Maximum thrust (vacuum/sea level) | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Specific Impulse - Vacuum For Shortest Firing (Cold) | Vacuum For Shortest Firing (Cold) | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Specific Impulse - Vacuum For Shortest Firing (Hot) | Vacuum For Shortest Firing (Hot) | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Total length | ft | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Engine diameter | x | x | Contractor | 1 | 1 | ||||||||||||||||||||
| Number of thrust chambers | x | x | Contractor | 1 | 1 | ||||||||||||||||||||
| Thrust chamber length | ft | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Thrust chamber diameter | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Nozzle length | ft | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Nozzle exit diameter | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Nozzle area ratio | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Engine cg from nozzle exit | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Position of engine mount from nozzle exit | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Mass of engine | x | x | Contractor | 1 | 1 | ||||||||||||||||||||
| Mass of thrust chamber | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Mass of nozzle | x | x | Contractor | 1 | 1 | ||||||||||||||||||||
| Mass of combustion chamber | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Pump mass (if any) | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Longitudinal moment of inertia of engine | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Lateral moment of inertia of engine | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Number of Coolant Passages | # | Number of Coolant Passages | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| FMAX | x | x | x | Contractor | 1 | 1 | |||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.3.2 | Solid Rocket Motors | ||||||||||||||||||||||||
| Number of Motors per Vehicle (values below are per motor) | # | Number of Motors per Vehicle (values below are per motor) | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Weight, Total | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Total impulse - Vacuum | lb-sec | Vacuum | Total impulse produced by motor. It is the product of thrust (at very high altitude (vacuum)) times duration over the motor burn time. | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Specific Impulse - Vacuum Average Over Burn Time | sec | Vacuum Average Over Burn Time | The thrust per unit propellant burned each second, it measures rocket performance and more specifically, internal thrust production a product of pressure and heat. | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Thrust - Vacuum Average Over Burn Time | lbs | Vacuum Average Over Burn Time | The average instantaneous force the motor produces during its burn. | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Burn Time | sec | The length of time from ignition of propellant to when all propellant has been consumed (the number of seconds for which the motor produces thrust). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Propellant Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Number of Nozzles | # | Number of Nozzles | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Propellant Material | Materials used in the construction of the item. | x | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Case Material | Materials used in the construction of the item. | x | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Nozzle Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Thrust Vector Control/Gimbal | Y/N | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| First Production Year | Year | First Production Year | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Man-Rated | Y/N | Is element man-rated? | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Number of Coolant Passages | # | Number of Coolant Passages | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Segmented | List | Yes | No | Contractor | 1 | 1 | |||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.3.3 | Propulsion Feed Systems | ||||||||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.4 | Mission Assurance Instrumentation | ||||||||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.5 | Reaction Control System | ||||||||||||||||||||||||
| Tank Diameter | ft | Physical measurement. | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Tank Length | ft | Physical measurement (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Tank Weight, Empty | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Tank Capacity | lbs | The Propulsion Liquid Rocket Engine's Fuel Tank Capacity. | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Pressurization | psi | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Primary Structural Material | Text | Materials used in the construction of the item. | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Cryogenic Contents | Y/N | Does element contain cryogenic contents? | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of Control Inputs and Outputs | # | Number of Control Inputs and Outputs | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Electronics Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Number Output Signals | # | Number Output Signals | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Power Input | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of Stages Covered | # | Number of Stages Covered | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| First Production Year | Year | First Production Year | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Manned Vehicle | Y/N | x | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| Nuclear Hardness | Y/N | Is element nuclear hardened? | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Power Dissipated | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.6 | Recovery System | ||||||||||||||||||||||||
| Parachute Size | Text | Size of parachute needed to support stage landing | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Flotation or Landing Gear | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Impact Resistency | x | x | Contractor | 2 | 2 | ||||||||||||||||||||
| Electronics Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Number Output Signals | # | Number Output Signals | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Power Input | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of Stages Covered | # | Number of Stages Covered | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| First Production Year | Year | First Production Year | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Manned Vehicle | Y/N | x | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| Nuclear Hardness | Y/N | Is element nuclear hardened? | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Power Dissipated | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.7 | Environmental Control System | ||||||||||||||||||||||||
| Number of Control Inputs and Outputs | # | Number of Control Inputs and Outputs | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Number of Pump Stages | # | Number of Pump Stages | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Electronics Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Number Output Signals | # | Number Output Signals | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Power Input | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of Stages Covered | # | Number of Stages Covered | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| First Production Year | Year | First Production Year | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Manned Vehicle | Y/N | x | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| Nuclear Hardness | Y/N | Is element nuclear hardened? | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Power Dissipated | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Electronics Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Number Output Signals | # | Number Output Signals | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Power Input | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.8.1 | Guidance navigation and Control | ||||||||||||||||||||||||
| G&C Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| G&C Power Consumption | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| G&C Volume | cu in | Physical measured size of the item. | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Orbital Insertion Error | x | x | Contractor | 3 | 3 | ||||||||||||||||||||
| Apogee Error | miles | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Target Apogee | miles | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Perigee Error | miles | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Target Perigee | miles | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Inclination Error | deg | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Target Inclination | deg | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Argument of Perigee Error | deg | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Target Argument of Perigee | deg | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Right Ascension of Ascending Node Error | deg | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Target RAAN | deg | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Spherical Error, Probable | miles | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Time of Flight | min | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Circular Error, Probable | miles | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Distance of Flight | miles | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Guidance Computer Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Guidance Computer Power Consumption | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Guidance Computer Volume | cu in | Physical measured size of the item. | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Processing Throughput | MIPS | x | x | Contractor | 2 | 2 | |||||||||||||||||||
| Memory Capacity | Kbytes | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Redundancy | % | x | x | Contractor | 3 | 3 | |||||||||||||||||||
| Number of Circuit Cards | # | Number of Circuit Cards | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Number of Control Inputs and Outputs | # | Number of Control Inputs and Outputs | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Power Dissipated | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Electronics Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Number Output Signals | # | Number Output Signals | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Power Input | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of Stages Covered | # | Number of Stages Covered | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| First Production Year | Year | First Production Year | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Manned Vehicle | Y/N | x | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| Nuclear Hardness | Y/N | Is element nuclear hardened? | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Gryo Type | List | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| Technology Readiness Level (TRL) | List | Technology Readiness Levels (TRL) are a method of estimating technology maturity of Critical Technology Elements (CTE) of a program during the acquisition process. Lookup TRL level values at bottom of the tab. | TRL 1 | TRL 2 | TRL 3 | TRL 4 | TRL 5 | TRL 6 | TRL 7 | TRL 8 | TRL 9 | x | x | x | x | Government | 1 | 1 | |||||||
| Manufacturing Readiness Level (MRL) | Text | Manufacturing Readiness Level (MRL) | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| 1.2.2.8.2 | Power | ||||||||||||||||||||||||
| Weight of Electrical Power System | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Volume of Electrical Power System | cu in | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Battery Capacity | Amp/Hr | Measure of the charge stored by the battery, and is determined by the mass of active material contained in the battery. The battery capacity represents the maximum amount of energy that can be extracted from the battery under certain specified conditions | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Total Launch Vehicle Cost Less Electrical Power | $K | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Number of Stages Covered | # | Number of Stages Covered | x | x | x | Contractor | 1 | 1 | |||||||||||||||||
| First Production Year | Year | First Production Year | x | x | x | Contractor | 2 | 2 | |||||||||||||||||
| Manned Vehicle | Y/N | x | x | x | x | x | Contractor | 1 | 1 | ||||||||||||||||
| Nuclear Hardness | Y/N | Is element nuclear hardened? | x | x | x | x | x | Contractor | 1 | 1 | |||||||||||||||
| Power Dissipated | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| Electronics Weight | lbs | Physical weight (use at least 1 decimal place). | x | x | Contractor | 1 | 1 | ||||||||||||||||||
| Number Output Signals | # | Number Output Signals | x | x | Contractor | 3 | 3 | ||||||||||||||||||
| Power Input | Watts | Physical weight (use at least 1 decimal place). | x | x | Contractor | 2 | 2 | ||||||||||||||||||
| New Design | Percentage | x | x | x | x | Contractor | 1 | 1 |
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