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FA8818-XX-X-XXXX

FA8818-XX-X-XXXX

PERFORMANCE-BASED WORK STATEMENT (PWS)

FOR

SMALL ROCKET PROGRAM-ORBITAL (SRP-O)

Mission: Tactically Responsive Launch – 3 and 4

Category 1 Mission Assurance

Basic: XX December 2020

REVISION HISTORY

REVISION
DATE
SECTION AFFECTED
COMMENTS

Table of Contents

1.0DESCRIPTION OF SERVICES/GENERAL INFORMATION4
1.1Scope and Objectives:4
1.2General Description of Services:4
1.3Management and Communications:4
1.4Systems Engineering (SE) Insight:4
1.4.1Entry Criteria:4
1.4.2Exit Criteria:5
1.5Cybersecurity:.5
1.5.1Unclassified Missions Requirements:5
1.5.2Controlled Unclassified Information (CUI):5
1.6Contractor Agreements and Non-Disclosure Agreements:6
1.6.1Associate Contractor Agreements (ACA):6
1.6.2Non-Disclosure Agreements:6
1.7Description of Services:6
1.8Mission Design, Integration, and Launch Service:7
1.8.1Mission Planning Service:7
1.8.2Periodic Interchange Meetings:8
1.8.3Formal and Government Reviews:8
1.8.4Formal Review Exceptions:8
1.8.5On-Site Government Representative(s):8
1.8.6Requirements Analysis and SRCR:8
1.8.7Mission Design:9
1.8.8Mission Build and Test:9
1.8.9Pre-ship Readiness Review (PSR) and Shipping:10
1.8.10Launch Campaign:10
1.9Mission Assurance Support Service:15
1.9.1Customer Analysis:15
2.0SERVICE SUMMARY –15
3.0DOCUMENTS18
3.1Reference Documents:18
3.2Compliance Documents:18
Annex 1: Performance Threshold Entrance and Exit Criteria19
Service Requirements and Concept Review (SRCR):19
Mission Design Review (MDR):20
Pedigree Review (PR):22
Pre-Ship Readiness Review (PSR)24
Appendix A: Mission Requirements Document (TacRL-3)26
Appendix B: Mission Requirements Document (TacRL-4)27

DESCRIPTION OF SERVICES/GENERAL INFORMATION

Scope and Objectives:

This PWS delineates the Launch Service Contractor (LSC) tasks required to perform launch operations and associated services necessary to conduct an orbital, Mission Assurance (MA) Category 1, mission in support of the Small Rocket Program-Orbital (SRP-O) Tactically Responsive Launch (TacRL) contract. The contracting agency is the Space and Missile Systems Center (SMC) Launch Systems Enterprise (SMC/ECL), Rocket Systems Launch Program (RSLP). Contractual direction is provided by the Procuring Contracting Officer (PCO), SMC/ADK, at Kirtland Air Force Base, New Mexico.

The objective of this program is to provide flexible small launch capability using Launch Vehicle (LV) designs based on commercial propulsion systems to meet a variety of mission and payload requirements. The specific mission objectives, satellite mission information, launch history requirements, and launch solution constraints are defined in the attached TacRL-3 and TacRL-4 Mission Requirements Documents (MRDs).

General Description of Services:

SMC requires launch services composed of design, integration, test, and launch activities as defined in this PWS and the MRD. A launch service is the totality of the launch vehicle and associated services required to meet the specific orbital launch objectives. This will include, but is not limited to, completion of design and development for any launch system designs that have not been previously qualified to mission levels, fabrication, test, and integration of the LV(s), all required LV support, integration of the LV with the payloads, and provision of launch facilities.

Management and Communications:

SMC will assign a Contracting Officer’s Representative (COR) to each contract awarded under this effort. This COR will act as the primary interface with the LSC and will provide Quality Assurance Surveillance on behalf of the PCO.

SMC will also assign a Mission Manager (MM) who will be responsible for leading an Integrated Product Team (IPT) to identify and manage the full breadth of mission planning and issues, including interfacing with the LSC to coordinate activities with customer and service provider stakeholders. The MM will typically coordinate these activities via a “Giver/Receiver” list, which reflects LSC deliverables defined in this contract and also captures stakeholder data requirements identified by the LSC.

The LSC shall structure its program coordination to provide clear, direct points of contact with the Government. The LSC shall communicate and coordinate program status, discussion of technical information, resolution of contract and financial issues, and provide meeting support.

Systems Engineering (SE) Insight:

The LSC shall employ a structured systems engineering approach to provide a reliable launch service. The Government will review this structured approach through the use of formal reviews. These reviews also serve as opportunities for the Government to conduct service performance surveillance as described in Section 1.3.

For all formal reviews, the LSC shall submit its evidence of performance.

Entry Criteria:

The entry evidence must meet the entry criteria specified for the review as detailed in Annex 2. Entry evidence shall be submitted thirty (30) calendar days (or earlier if available) in advance of the review event. The Government Red Team of subject matter experts (SMEs) will perform a technical evaluation of the evidence submitted and determine whether the evidence demonstrates the LSC is prepared to conduct the formal review. The COR will communicate the determination of the Government no later than seven (7) calendar days prior to the review. [CDRL A002] Exit Criteria:

The COR will communicate any formal review deficiencies, commonly referred to as “liens,” to the LSC at the close of the review. Liens will be validated by the COR and considered by the PCO in the determination that the relevant service has been satisfactorily performed.

The LSC is responsible for collecting, logging, disseminating and assigning resources for responding to each lien, and other action items, identified at the review. The LSC will provide a get-well plan, which includes a burn-down plan and schedule to remedy deficiencies to the COR no later than seven (7) calendar days after the review. Closure dates will be agreed to by the COR and the LSC. [CDRL A002] Cybersecurity: Classification requirements for the mission will be specified in the MRD.

Unclassified Missions Requirements:

The LSC shall obtain range authority to connect approval(s) for all commercial information systems planned to support the launch.

Controlled Unclassified Information (CUI):

CUI provided under this contract shall be managed and safeguarded IAW DoDM 5200.01, V4, Controlled Unclassified Information.

Protection of Unclassified DoD Information on Non-Government Information Systems: The Contractor must comply with the information safeguards as specified in DoDI 8582.01, Security of Unclassified DOD Information on Non-DOD Information Systems, CNSSP No. 18, National Policy on Classified Information Spillage, Chairman of The Joint Chiefs of Staff Instruction (CJCSI) 6510.01, Information Assurance and Support to Computer Network Defense (CND), and AF Manual 17-1301, Computer Security.

The Contractor shall comply with DFAR Clauses related to the Disclosure of Information (DFAR 252.204-7000), Safeguarding Covered Defense Information and Cyber Incident Report (DFARS 252.204-7012 and DFAR Subpart 204.73) for the protection of unclassified controlled technical information (UCTI).

In line with this clause, NIST SP 800-171 provides guidance for the protection of Controlled Unclassified Information (CUI) on non-federal information systems. Contractor shall apply security controls contained in NIST SP 800-171 for the protection of CUI on non-DoD information systems. CUI information will not be placed on publicly accessible web sites.

Public release is a security and policy review of all official, and some unofficial, DoD information intended for release to the public when that information is about military matters, national security issues, or subjects of significant concern to DoD or AF. All unclassified information, such as papers, presentations, videos, images and news releases, must be reviewed before it’s released to the public. Any and all release requests will be requested by the LSC through the PCO.

Contractor Agreements and Non-Disclosure Agreements:

Associate Contractor Agreements (ACA):

The LSC shall enter into ACAs for any portion of the contract requiring joint participation in the accomplishment of the Government’s requirement(s). These agreements shall include the basis for sharing information, data, technical knowledge, expertise, and/or resources essential to the conduct of the mission, which shall ensure the greatest degree of cooperation for the development of the program to meet the terms of the contract. Since the associate contractors will vary by mission, they will be listed in the MRD.

ACAs shall include the following general information:

· Identify the associate contractors and their relationships.

· Identify the program involved and the relevant Government contracts of the associate contractors.

· Describe the associate contractor interfaces by general subject matter.

· Specify the categories of information to be exchanged or support to be provided.

· Include the expiration date (or event) of the ACA.

· Identify potential conflicts between relevant Government contracts and the ACA; include agreements on protection of proprietary data and restrictions on employees.

A copy of such agreement shall be provided to the PCO for review before execution of the document by the cooperating contractors.

The LSC is not relieved of any contract requirements or entitled to any adjustments to the contract terms because of a failure to resolve a disagreement with an associate contractor. Liability for the improper disclosure of any proprietary data contained in or referenced by any agreement shall rest with the parties to the agreement, and not the Government. All costs associated with the agreements are included in the negotiated prices of applicable orders issued under this contract. Agreements may be amended as required by the Government during the performance of this contract.

Non-Disclosure Agreements:

The LSC shall establish Non-Disclosure Agreements with other contractors performing related services for the Government, such as SV Contractors who may be responsible for payload operations, and Mission Assurance Contractors (MAC) who may perform Independent Verification and Validation (IV&V) activities on behalf of the Government.

Description of Services:

The LSC shall perform the services described in this PWS as specified in the MRD. Services and review events are summarized in Figure 1 below.

Figure 1: SRP-O Contract Services (SE Events Based on Notional 12 Month Timeline)

Mission Design, Integration, and Launch Service:

The LSC shall complete design and development of the mission launch solution, conduct mission trade studies and mission design, complete fabrication/integration, payload integration and testing of the LV and supporting systems, and execute the launch including post flight analysis.

Mission Planning Service:

The LSC shall develop and maintain a CWBS, CWBS Dictionary and an Integrated Schedule (IS) for the mission. The CWBS, CWBS Dictionary and IS shall reflect all the tasks/activities planned for the mission using a common numbering system. Tasks/activities shall be logically linked together and show predecessor/successor relationships and establish the logical flow of dates provided by calculating the duration of all tasks using typical schedule networking tools. The IS shall be presented at formal reviews at a sufficiently detailed level to display milestones and primary processes of interest. [CDRL A019, A027] The CWBS shall reflect the LSC’s overall view of the effort and serve as the framework for organizing activities involving the LSC and their subcontractors, Government, Range and Associated Contractors (refer to MIL-HDBK-881D Appendix I for a sample CWBS showing typical levels).

The CWBS Dictionary shall define the tasks to be performed in each element of the CWBS and corresponding element of the IS. This task definition shall include a complete definition of the task to be accomplished, the key processes, procedures and specifications to be used when performing the task and the CDRL item(s) to be delivered.

The IS shall reflect all the tasks/activities in the CWBS, and include all applicable PWS tasks. Tasks/activities shall be logically linked together and show predecessor/successor relationships and establish the logical flow of dates provided by calculating the duration of all tasks using typical schedule networking tools. The IS shall display the critical path as well as schedule margin and deviation. The IS shall be maintained and updated no less than monthly. The IS shall reflect all planned mission activities, including external dependencies.

Periodic Interchange Meetings:

The LSC shall support weekly meetings of the Government IPT led by the Government COR and/or MM. The LSC shall support any working group designated to address specific mission issues of concern that require the combined attention of the Government, supporting contractors, and LSC. The LSC shall support daily telecons during the launch campaign. [CDRL A018] The LSC shall host and conduct a mission kickoff meeting, at LSC facility, with government representatives within 14 calendar days of contract award.

Formal and Government Reviews:

To provide the Government with opportunities for performance surveillance and insight into the processes, methodology and progress being made by the LSC, the following formal reviews shall be hosted at the LSC’s facility [CDRL A018]:

Formal Reviews

· Service Requirements and Concept Review (SRCR)

· Mission Design Review (MDR)

· Pedigree Review (PR)

· Pre-ship Readiness Review (PSR) Government Reviews

· Mission Readiness Review (MRR)

· Flight Readiness Review (FRR)

· Launch Readiness Review (LRR) Formal Review Exceptions:

The timing of these reviews shall be agreed upon by the COR and the LSC. Reviews may be waived by the COR if they are deemed of low value to the mission. The COR may also combine reviews for the sake of cost and efficiency.

On-Site Government Representative(s):

Not required.

Requirements Analysis and SRCR:

The LSC shall perform requirements analysis for the specific mission; including mission requirements decomposition, allocation and validation of PWS and MRD requirements. The LSC shall specify system performance. [CDRL A001] A Requirements Traceability and Verification Matrix (RTVM) documenting how requirements are derived and verified and specifying artifacts required to demonstrate verification shall be maintained throughout the life of the contract. [CDRL A021] At the conclusion of the requirements analysis (no later than 90 calendar days after contract award or as directed by the COR) the LSC shall hold an SRCR to present the results of requirements analysis and the mission design concept. [CDRL A002] Mission Design:

The LSC shall perform mission design for the specific mission. In this activity the LSC designs the complete mission launch solution. The launch schedule will be driven by SMC/ECLX.

Interface Control Document (ICD):

The LSC shall create, maintain configuration control and coordinate the ICD change process throughout the life of a contract. The ICDs shall be generated to document the interfaces between the LV and the payload, and the Integration/Launch Site (ILS)/Range. The LV to ILS/Range ICD shall include a description of the telemetry data to be displayed on range consoles. [CDRL A004] Space Debris Assessment Report (SDAR):

The LSC shall perform analysis and produce a SDAR to demonstrate compliance with AFI 91-202 for the LV (the SV shall not be included in this report/analysis). [CDRL A015]

MDR:

At the conclusion of the mission design phase (approximately T-6 months to launch or as directed to by the COR) the LSC shall hold an MDR. The objective of the MDR is to demonstrate critical design of any design items that were proposed as only developed to the preliminary design level, and to demonstrate a full mission design that the system satisfies. [CDRL A002, A018] Pedigree Review (PR):

The LSC shall host a PR at approximately T-70 days to launch (or as approved by the COR). The main purpose of a PR is to ensure that the flight hardware/software has been built and satisfactorily tested to establish flight worthiness in accordance with the released design qualification documentation. [CDRL A024] Mission Build and Test:

The LSC shall fabricate and test hardware and software to ensure that the Government is provided a launch solution design capable of meeting all the requirements of the SRP-O contract PWS and MRD.

Coupled Loads Analyses (CLA):

CLAs shall be performed by the LSC to predict the maximum loads that can be expected by the payload during the launch event. The CLA will address key loading events (e.g. lift-off, maximum dynamic pressure, transonic, staging/ignition events, engine cut-offs and restarts, and steady state conditions, as applicable). The preliminary CLA shall be performed based upon preliminary payload-provided models to support payload design and test programs. A final CLA shall be performed with test verified models. [CDRL A015] Predicted Environments:

The LSC shall generate predicted launch environments based upon mission development activities. The LSC shall ensure that the predicted environments meet the requirements stated in the MRD and ICD. The LSC shall be responsible for any changes required to the LV to meet these requirements. [CDRL A015] Fabricate & Test:

The LSC shall develop, fabricate and test flight hardware and flight software, necessary to conduct the mission described in the MRD. The LSC shall conduct hardware and software system level testing to meet acceptance and qualification requirements. Flight hardware and software shall be fabricated and developed under configuration control. All work performed under this effort shall be performed in accordance with the LSC’s processes, procedures and LV specifications.

Pre-ship Readiness Review (PSR) and Shipping:

The PSR must be completed prior to shipping major LV components or support equipment to the ILS so that the Government and other launch campaign stakeholders may assess LSC launch campaign readiness and schedule risk prior to committing resources to the campaign. The PSR will be held at approximately T-60 days to launch or as directed to by the COR. The LSC is responsible for shipment and/or transportation of all LV hardware, Ground Support Equipment (GSE), Launch Support Equipment (LSE) and other necessary items to the ILS. If directed by the Government, the program and LSC will coordinate military air transport (MILAIR) of specified equipment at Government expense. [CDRL A002] LV / Payload Mechanical Interface Verification.

A mechanical fit check shall be performed to verify the compatibility between the LV and the payload separation system as documented in the LV/Payload ICD, including cable routing and connections and any areas where there are potential interference issues. The LSC and the separation system provider shall provide flight representative hardware to support the fit check. The fit check shall be performed at an LSC provided facility or the agreed upon alternate facility.

LV / Payload Electrical Interface Verification:

End-to-end testing shall be conducted to verify the electrical interface between the LV and SV(s). The testing shall use flight-representative hardware furnished by the LSC as well as applicable SV(s) components furnished by the SV(s) and/or separation system contractor. The test(s) shall include the complete exercise of all electrical interfaces between the LV, separation system and the SV(s). Integrated test procedures shall be reviewed and approved by participating agencies. The location of the test will be proposed by the LSC. [CDRL A012] Readiness:

At the PSR, the LSC shall provide an overview demonstrating completion of the Range Safety preparations and tailoring (if required), an acceptable approach to Flight Safety and Flight Termination, and readiness of the ILS and support facilities. The LSC shall also demonstrate that system level testing has been completed and the LV hardware is prepared for shipment to the ILS.

Launch Campaign:

The LSC shall execute the launch campaign, coordinate all safety operations with the Range and ensure that critical skills and qualified personnel are available when required for integration, testing and on-console operations. The LSC shall also provide calibrated, certified and qualified LSE and GSE as required for the completion of range integration tasks to process, prepare and launch the LV with the integrated payload(s). This activity requires close cooperation between the Government, LSC, payload provider and the Range.

ILS and Services:

The Government will provide Government services at Government ranges (e.g., Flight Safety, Telemetry, Radar, etc.). The LSC shall specify all required Government range services/support. All spaceport services, non-Government range services and ILS services shall be provided by the LSC, unless otherwise stated in the MRD. [CDRL A010] Range Requirements Coordination and Documentation:

The LSC shall comply with Range processes to ensure that the requirements specified in the PWS and MRD are safely executed and properly coordinated with the Range. The LSC is responsible for obtaining, producing and/or coordinating all items required by the Range. The LSC shall develop and provide Universal Documentation System (UDS), or other range-required documentation inputs for submittal by the program office to the Range as required by the ILS. The LSC shall participate in Range working groups as required. [CDRL A010] Range Safety:

The LSC shall comply with 14 CFR Part 417 (or equivalent, when specified by the cognizant range) for all applicable ILS activities. These safety requirements may be tailored by the LSC, as detailed below. The LSC is responsible for obtaining approval for range safety tailoring. The LSC shall coordinate scheduling all activities and/or operations with the Range Safety Office, as applicable. [CDRL A010, A020] Ground and Flight Safety Hazard Analyses:

Ground and flight safety hazard analyses shall be performed by the LSC in accordance with 14 CFR Part 417 (or equivalent when specified by the cognizant Range).

The LSC shall work with the cognizant range safety office in coordination with program office to tailor the applicable flight safety requirements for the launch system, complete development of a compliant flight safety system and gain range safety approval for the implementation of its flight safety system (if required). The LSC shall make prompt waiver requests to the COR if unable to meet range safety requirements due to technical issues with the design or flight hardware. Failure to obtain approval for the desired tailoring shall not relieve the LSC of its responsibilities under this contract. [CDRL A010, A020] Safety and Environmental:

The LSC shall support the Government safety and environmental reporting required for safety, hazards, debris, and environmental analysis. [CDRL A020] Facilities and Services:

The LSC shall provide the required facilities and services at the ILS, which meet all mission requirements defined in the MRD and this PWS unless otherwise stated in the MRD. These requirements shall include, but are not limited to, safety, contamination control, payload integration, flight control facilities, transportation, lifting/stacking and fueling infrastructure, unless otherwise specified. The Payload Processing Facility (capable of accommodating LSC encapsulation activities) will be provided by the SV contractor unless otherwise stated in the MRD.

Approvals and Waivers:

The LSC shall obtain any necessary coordination or approval from the launch base or test range for activities taking place at the launch base or test range. The LSC shall obtain appropriate documentation, approvals, and perform other necessary actions to secure access to equipment, facilities, etc. If waivers are required, the LSC shall obtain them prior to initiating facility activation or modification. Equivalent levels of safety requests shall be briefed at range working groups and formal reviews. The LSC's failure to gain a required approval or waiver shall not relieve the LSC of any responsibilities under this contract. If the LSC identifies any work outside the scope of this contract that is required to meet range requirements, the LSC shall immediately notify the PCO. [CDRL A010] New Strategic Arms Reduction Treaty (START) Requirements:

GFP motors subject to New START considerations will not be provided for this effort.

Classified Payloads:

When classified payloads are processed, the LSC shall provide trained people with the proper clearance to perform the required work in compliance with the applicable Security Classification Guide (SCG). Classification requirements for each mission will be specified in the MRD and associated mission specific DD254.

LV/Payload Operations:

The LSC shall integrate the payload(s) with the LV in a clean room environment as specified in the MRD, and perform end-to-end testing with the payload(s). End-to-end verifications tests are tests of the hardware/software to obtain or validate engineering data on the performance of the system prior to the execution of the launch operation. [CDRL A012] Launch Verification Testing:

An integrated field processing procedure shall be prepared by the LSC test conductor in each test. All anomalies shall be documented by the LSC. [CDRL A012] LV/Payload Mating:

Unless otherwise specified in the MRD, the SV Contractor will be responsible for all payload integration activities prior to integrated operations. During payload mating, the SV Contractor will furnish certified handling/GSE required to interface from the crane hook (or other GSE) to the payload, as required during the integration process. The SV Contractor will transfer responsibility for the payload to the LSC when the payload is fully prepared for immediate mating with the LV, and is approximately three inches away from the LV mating surfaces. The LSC shall conduct mechanical mating, spurious voltage, and electrical connection checks in concert with the SV Contractor.

LV/Payload Integrated Processing:

Integrated LV/payload processing shall be performed in preparation for payload emplacement on the LV at the ILS. The LSC shall accommodate the payload GSE at the ILS. The LSC shall assist the SV Contractor in conducting post-mate checks that may include the payload operational assurance tests and a compatibility test of the LV and payload systems, and the GSE interfaces.

Payload Flight Integration Tests:

The flight integration test shall be performed using the flight hardware to verify electrical compatibility and system performance between the payload and the LV upper section(s) prior to movement to the ILS (typically performed within a processing facility at the launch range). Integrated operations will be performed using procedures approved by participating agencies. The LSC shall provide hardware for any LV-required tests, and the SV Contractor will provide hardware for any payload-required tests.

Payload Support Equipment and Ground System Checkout:

The SV Contractor will install the required payload support equipment at the ILS in locations to be defined in the LV/Payload ICD. A design compatibility test to establish high confidence in electrical compatibility of the payload and payload GSE with the launch complex will be performed at the ILS. The payload provider will prepare the test procedure and conduct the test. The LSC shall provide support personnel and the SV Contractor will supply all payload - related GSE. The LSC shall provide support to the SV Contractor to test the installed equipment.

Simulations & Rehearsals:

The LSC shall coordinate and conduct mission simulations and dress rehearsals in accordance with their proposed approach. The LSC shall compile mission launch notebook data and identify corrections based on these simulations and rehearsals. [CDRL A016] Mission Constraints:

The LSC shall compile all payload and LV launch constraints, and coordinate these with the MM prior to inclusion in the mission launch notebook data. [CDRL A016] Launch Activities:

The LSC shall prepare the LV for launch, conduct prelaunch checkout, conduct launch operations, ensure the collection and recording of telemetry during the launch, support post launch mission activities, perform post-flight analysis, and conduct site shutdown. During the launch campaign, the LSC shall identify all daily planned activities to the MM.

Nets and Telemetry:

The LSC shall provide the Government with access to all voice (transmit and receive), video, and data networks used for launch support. At Government ranges, the LSC shall provide requirements for range and downrange telemetry collection via the UDS process. [CDRL A016] Day of Launch:

The LSC shall be responsible for Day of Launch operations and the final readiness decision for the combined LV/payload system. The LSC shall accommodate a small contingent of no more than six (6) Government personnel to monitor launch operations for Government insight. The Government will not have a Mission Director or have an approval role in the launch decision.

The LSC shall accommodate payload personnel on console. The LSC shall not launch if the payload lead informs the LSC of non-readiness to launch during the final poll for launch readiness.

The LSC shall provide trajectory and covariance data to support Joint Space Operations Center (JSPOC) and Safety collision avoidance calculations. [CDRL A015] The LSC shall define an LV instrumentation approach (type and model, function, location, orientation (if applicable), and data retention) [CDRL A016].

Post-Flight Activities:

The LSC shall conduct an analysis of and participate in a review of operations, flight telemetry, and other data to determine LV performance.

Quicklook Analysis:

The LSC shall develop the T+4 hours (Quicklook) analysis. Analysis shall include characterization of trajectory/orbit insertion parameters, mission timeline/events, environments, telemetry performance, observations and anomalies. [CDRL A017] Lessons Learned:

The LSC shall collect lessons learned throughout the performance of the contract and support the Governments IPT lessons learned process. [CDRL A017] Post-Flight Analysis:

The LSC shall complete the post-flight analysis by L+4 days and L+30 days. The LSC shall attend and support a Government post flight review at SMC (Los Angeles, CA) at approximately L+60 days. [CDRL A017] Failure Review:

In the event of a complete or partial mission failure, the LSC shall participate in a Government-led evaluation of the root cause of the failure event to identify remedial actions required to prevent recurrence. Mission failure reviews will be conducted in accordance with FAA license procedures. The LSC shall enable Government access to all internal investigations of anomalies and failures. [CDRL A014] Mission Assurance Support Service:

The LSC shall conduct mission assurance (MA) in accordance with its proposed internal processes and procedures. The mission is not subject to the SMC flight worthiness certification process or MAC IV&V activities, but will rather be licensed under Federal Aviation Administration (FAA) licensing guidelines.

The LSC shall obtain an FAA launch license and is responsible for all requirements to obtain such license. LSC shall also obtain launch vehicle frequency clearance from the Federal Communications Commission (FCC) or equivalent. The LSC shall submit a copy of the approved license(s) and all supporting documentation. [CDRL A010] In addition, the LSC shall be responsible for ensuring the applicable ILS meets FAA licensing requirements and any activities required to bring the ILS into licensing compliance. This LSC shall demonstrate that all required FAA licenses have been obtained at the PSR. Obtaining applicable licenses shall not relieve the LSC from the requirements described in paragraph 1.8. Failure to obtain applicable licenses shall not relieve the LSC from its responsibilities under this contract.

Customer Analysis:

The following analyses shall be conducted to support payload integration:

Payload Trajectory and Performance Analysis [A015] RF Analysis (including intermodulation analysis) [A015] Antenna Patterns and Link Analyses [A015] Re-Contact Analysis [A015]

SERVICE SUMMARY –

The COR for the launch service contract will perform surveillance of the service provided. The table below provides an overview of the performance thresholds the COR will employ to evaluate the services provided. For services where the threshold incorporates validated complaints, the COR will solicit positive and negative feedback from designated stakeholders and validate any complaints as part of the service evaluation. The COR will assess the quality of each service provided and make a final recommendation to the PCO for determination of the acceptability of the service rendered.

Table 1 - Service Summary

SS #
Performance Category
PWS Paragraph
Performance Threshold
1
Launch Service
1.8
See Below
1.1
Requirements Analysis
1.8.6

Entry: <3 findings of non-readiness against the SRCR entry criteria as determined by the COR, corrected in one cycle.

Exit: <3 liens against the SRCR exit criteria as determined by the COR.

Schedule: This review shall be completed no more than 90 days after contract kickoff or as determined by the COR.

1.2
Mission Design
1.8.7

and Sub-paragraphs

Entry: <3 findings of non-readiness against the MDR entry criteria as determined by the COR, corrected in one cycle.

Exit: <3 liens against the MDR exit criteria as determined by the COR.

Schedule: Completion of flight safety requirements tailoring prior to MDR.

Schedule: MDR shall be completed approximately T-6 months to launch or as directed to by the COR.

1.3
Mission Build and Test
1.8.8

and Sub-paragraphs

Entry: <3 findings of non-readiness against the PSR entry criteria as determined by the COR, corrected in one cycle.

Exit: <3 liens against the PSR exit criteria as determined by the COR.

Schedule: Secure all required FAA license(s) (as required) and Completion of SFWC inputs prior to PSR.

Schedule: Completion of PSR within 30 days of IS-reflected date as of MDR, unless otherwise specified by the COR.

1.4
Launch Campaign
1.8.10

and Sub-paragraphs

Performance: LSC support equipment & logistics will be available and meet all mission requirements.

Schedule: No more than 14 days of LSC-driven launch delays (per schedule as of PSR).

Performance: No more than 3 validated complaints from the cognizant flight safety office. No more than 3 validated complaints from the launch range ground safety office. No more than 3 validated complaints by the payload provider.

Performance: Insertion of payload(s) into designated trajectory within tolerances specified in the MRD.

Note: PCO is the unilateral authority for validation of complaints discussed above.

DOCUMENTS

Reference Documents:

The following documents are to be considered as reference material for the purpose of interpreting the requirements of this PWS but are not contractual documents.

Document Number
Document Title
Comments
AFMAN 91201
Explosives Safety Standards, 21 MAR 17
MIL-HDBK-881C
Work Breakdown Structures for Defense Materiel Items
SMC-G-1204
SMC Readiness Review Process
SMC-S-001
Systems Engineering Requirements and Products
MIL-STD-961E
Defense and Program-unique Specifications Format and Content
LTS 10-2010-04
Test Requirements for Launch Vehicles
Tailored RSLP Version of SMC-S-016 Test Requirements For Launch, Upper- Stage, & Space Vehicles which is by itself a tailored version of MIL-STD-1540E

Compliance Documents:

All launch related services require compliance with the governing regulations and laws affecting the procurement and execution of launch services. Compliance with the following is mandatory.

Document Number
Document Title
Comments
14 CFR Part 415
FAA Launch License
Or as directed by cognizant Range.
14 CFR Part 417
FAA Launch Safety
14 CFR Part 431
FAA Launch and Reentry of a Reusable Launch Vehicle
If applicable
DOD 4145.26-M
DOD Contractor’s Safety Manual For Ammunition and Explosives
No pre-award survey required; applicable only for contractors handling explosives.
DoD 5220.22-M
National Industrial Security Program Operating Manual
AFI 91-202
US Air Force Mishap Prevention Program, 12 Mar 2020

Annex 1: Performance Threshold Entrance and Exit Criteria Service Requirements and Concept Review (SRCR):

Entrance Criteria

Description
CDRL#
Due

1. Coordinated and signature ready System Performance Specification (PWS 1.8.6) (Updates as necessary for subsequent reviews)

A001
Draft: SRCR-30d

Final Rev: SRCR

2. Integrated Schedule (PWS 1.8.1)
A027
Monthly – Most recent version to be included with Review submission at SRCR-30d
3. Preliminary RTVM (SPS RTVM, PWS RTVM, MRD RTVM) (PWS 1.8.6)
A021
SRCR-30d
4. Initial submittal of System Safety Program Plan (SSPP) (PWS 1.8.10.3)
A020
SRCR-30d

5. Draft SRCR briefing chart package, Design Review Information Package (DRIP) review charts that include (PWS 1.4.1, 1.8.6):

a. Overview of the proposed Mission concept

b. Proposed LV design

c. Assessment of compliance with requirements

d. Current integrated schedule and critical path

e. Planned trade studies

f. Proposed plan for submittal of all required contract deliverables including projected submittal dates

g. Initial risk assessment and mitigation plan presented (including first flight items)

h. Proposed logistics concept

i. Safety program

j. Proposed plan for compliance with Range Interface and Range Safety requirements

k. Schedule and status of all range documents

l. Path ahead to MDR outlined

A002
SRCR-30d

Rev: SRCR-5d

Exit Criteria

Description
CDRL#
Due
1. Review of action items with assignee and closure dates (PWS 1.4.2)
A018
NLT SRCR+7d
2. Final SRCR briefing chart package (PWS 1.8.3)
A002
SRCR
3. SRCR get well plan/schedule to close any liens (PWS 1.4.2)
A002
SRCR+7d

Mission Design Review (MDR):

Entrance Criteria

Description
CDRL#
Due

1. All liens and action items from SRCR completed and closed out

2. Updated Integrated Schedule (PWS 1.8.1)
A027
Monthly – Most recent version to be included with Review submission at MDR-30d
3. Updated RTVM (SPS RTVM, PWS RTVM, MRD RTVM) (PWS 1.8.6)
A021
Rev: MDR-30d
4. Coordinated and signature ready ICDs (PWS 1.8.7.1)
A004
MDR-15d

Signed: MDR+30

5. Schedule and status of all range documents
A010
MDR-30d
6. Draft Range Safety documents (PWS 1.8.10.3)
A010
MDR-30d
7. FAA license package complete with all attachments (PWS 1.9)
A010
MDR-30d
8. FCC license package complete with all attachments (PWS 1.9)
A010
MDR-30d
9. System Safety Program Plan (PWS 1.8.10.3)
A020
Revision: MDR-30d

Final: MDR+10d

10. Preliminary Safety Assessment Report (PWS 1.8.10.4.1)
A020
MDR-30d

Final: Haz Ops-30d

11. Integrated Field Processing Procedures (PWS 1.8.10.9.1)
A012
Draft: MDR-30d

Final: Test-7d

12. Draft MDR briefing chart package, Design Review Information Package (DRIP) review charts that include (PWS 1.4.1):

a. Final trade study results

b. Current integrated schedule and critical path

c. Assessment of requirements compliance

d. Proposed plan for submittal of all required contract deliverables including projected submittal dates

e. Planned and completed qualification and acceptance testing

f. Updated risk and opportunity assessment and mitigation

g. Status of long lead items and critical spares procurement

h. All system safety and range safety issues addressed, and status of documents briefed

i. Proposed plan for compliance with Range Interface and Range Safety requirements

j. Path ahead to PSR outlined

A002
MDR-30d

Rev MDR-5d

Description
CDRL#
Due
1. Review of action items with assignee and closure dates (PWS 1.4.2)
A018
NLT MDR+7d
2. Final MDR briefing chart package (PWS 1.8.3)
A002
MDR
3. MDR get well plan/schedule to close any liens (PWS 1.4.2)
A002
MDR+7d

Pedigree Review (PR):

Entrance Criteria (documentation for each of the following is provided for review)

Description
CDRL#
Due
1. Acceptance testing of subassemblies and/or components (PWS 1.8.7.4)
A024
PR-30d
2. Factory system level testing including payload integration tests
A024
PR-30d
3. Documentation that all LV and GSE systems have been fabricated and assembled as designed, including documentation of rationale for deltas
A024
PR-30d
4. Mechanical top assembly drawings, with parts list and sub-tier drawings necessary to locate all major units on the vehicle, including mounting configuration (hard mounted or on isolators)
A024
PR-30d
5. Component qualification matrix with the test spectra and levels (thermal cycle, vacuum/thermal vacuum, random vibration, sine vibration, shock, and EMI) to which each component has been qualified
A024
PR-30d
6. Qualification and Acceptance test data and reports including lot qualification data on ordnance
A024
PR-30d
7. Component service life data and manufacturing dates on ordnance and other limited life items are documented and within service life
A024
PR-30d
8. Qualification by similarity analyses and reports
A024
PR-30d
9. Documentation/analyses used as basis for qualification and acceptance test levels
A024
PR-30d
10. All Discrepancy Reports (DRs) and referenced documents as well as a complete summary listing. A reduced set of DRs, deemed engineering significant by the review team, may be requested after review of the DR list and description
A024
PR-30d
11. Documentation of concurrence/approval on all DRs
A024
PR-30d
12. Documentation of concurrence/approval on all waivers and deviations including a summary listing
A024
PR-30d
13. Copies of waivers granted to the system, or in-process
A024
PR-30d
14. GIDEP alerts and other advisories and how they were addressed
A024
PR-30d
15. Current ICDs and signed off documentation
A024
PR-30d
16. Documentation of Software development and mission specific software test and qualification
A024
PR-30d
17. LSC’s qualification, acceptance, and non-complying product process documentation, including acceptance test reports for all LSC fabricated and vendor supplied components (mechanical and electrical, software if applicable) and subassemblies
A024
PR-30d
18. Acceptance level test results
A024
PR-30d
19. System level test results
A024
PR-30d
20. Build paperwork and travelers (Provided for review at LSC facility at PR)
A024
PR-30d
21. Limited-life items documentation of service life
A024
PR-30d
22. Documentation of Fatigue analysis showing component fatigue life remaining after exposure to environmental tests
A024
PR-30d
23. Critical connections list showing all connections that cannot be tested after final mating
A024
PR-30d
24. Launch system electrical interconnect drawing(s), including Cable Layout Drawings showing proper routing of all cables
A024
PR-30d
Description
CDRL#
Due
1. Review of action items and Requests for Information (RFIs) with assignee and closure dates (PWS 1.4.2)
A018
NLT PR+7d
2. LSC’s responses to all RFIs (PWS 1.8.3)
A018
PR+7d

Pre-Ship Readiness Review (PSR) Entrance Criteria

Description
CDRL#
Due

1. All action items / liens from MDR closed

2. Integrated Schedule (PWS 1.8.1.3)
A027
Monthly – Most recent version to be included with Review submission at PSR-30d

3. All hardware to be shipped has been verified available and mission ready

4. All field processing procedures released (PWS 1.8.10.9.1)
A012
PSR-30d
5. Safety Assessment Report complete (PWS 1.8.10.4.1)
A020
Final: Haz Ops-30d
6. Schedule and status of all range documents
A010
PSR-30d
7. Final, Signed Range Safety documents (PWS 1.8.10.3)
A010
PSR-30d
8. FAA License(s) Approved (PWS 1.9)
A010
PSR-30d
9. FCC License(s) Approved (PWS 1.9)
A010
PSR-30d
10. All Radio Frequency (RF) documents approved (PWS 1.9.1.2)
A015
PSR-30d

11. For any open non-compliances, closure dates identified and approved to proceed with shipment to the field

PSR-30d

12. Path ahead to ILC outlined

PSR-30d

13. Draft PSR briefing chart package (PWS 1.4.1)

a. Mission specific requirements and analyses reviewed

b. Final Compliance Verification Matrices reviewed

c. Hardware qualification and acceptance testing completed and reviewed

d. System Testing complete and reviewed

e. Flight software testing completed

f. Risk mitigation status reviewed

g. Status of range safety approvals reviewed

h. Documentation of Range readiness reviewed

i. All licensing approved (exceptions noted – to be carried as risks)

j. Launch Campaign Concept of Operations (CONOPS) reviewed

k. Launch Campaign daily schedule reviewed

A002
PSR-30d

Rev PSR-5d

14. Final RTVM (SPS RTVM, PWS RTVM, MRD RTVM) (PWS 1.8.6)
A021
PSR-30d
15. Customer Analyses Reports (PWS 1.9.1)
A015
Final: PSR-30d
Description
CDRL#
Due
1. Review of action items with assignee and closure dates (PWS 1.4.2)
A018
NLT PSR+7d
2. Final PSR briefing chart package (PWS 1.8.3)
A002
PSR
3. PSR get well plan/schedule to close any liens (PWS 1.4.2)
A002
PSR+7d

SRP-O – Cat 1 PWS – XX Dec 2020 Page 7 of 27 Appendix A: Mission Requirements Document (TacRL-3)

Appendix B: Mission Requirements Document (TacRL-4) image2.png image3.jpeg image1.png

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