Attachment 3 Spacecraft and Ground Technical Specification Sheet (SGTSS) 8 Sept 2022.xlsx

XLSX spreadsheet 30 KB Posted

Attached to
DRAFT RFP - Space Test Experiment Platform (STEP) 2. 0- AMENDMENT 2 Federal contract opportunity
Solicitation number
FA881822R0003
Issued by
Department of the Air Force Space Command Space and Missile Systems Center

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Other files for this federal contract opportunity

Other files attached to DRAFT RFP - Space Test Experiment Platform (STEP) 2. 0- AMENDMENT 2, newest first.
File Type Posted
STEP 2.0 Industry Day Special Announcement AMENDMENT 2.pdf PDF
Attachment 1 Statement of Work (SOW) v2.docx DOCX document
Attachment 4 DD254 v2.pdf PDF
Attachment 4 DD254.pdf PDF
FA881822R0003 DRAFT Request for Proposal 13 Oct 2022.pdf PDF
Attachment 1 Statement of Work (SOW).docx DOCX document
Attachment 2 Systems Requirement Document (SRD).docx DOCX document
Attachment 8 Comment Resolution Matrix (CRM).xlsx XLSX spreadsheet
Exhibit A Contract Data Requirements List (CDRL).pdf PDF
Attachment 7 Cost and Software Data Reporting Plan.xlsx XLSX spreadsheet
Attachment 10 Past Performance Questionnaire 14 Sept 2022.pdf PDF
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Sheet1

ID UNITS PERFORMANCE OR DESCRIPTION

(alphanumeric)

SPACE VEHICLE PERFORMANCE
1.1LAUNCH VEHICLE COMPATIBILITY
1.1.1Reference Launch Vehicle Configuration (last LV used)
1.1.2SV-LV Attach Fitting
1.1.3Fairing Diameter (last LV used)
1.1.4Other Launch Vehicle Compatibilitiy's
1.1.5Prior Most Severe Vibration Environment
1.1.xOther
1.2REFERENCE ORBIT COMPATIBILITY
1.2.1Apogee Altitude Range(km)
1.2.2Perigee Altitude Range(km)
1.2.3Inclination Range(deg)
1.2.4Other Orbit Compatibility's
1.2.5End-of-life Capability
1.2.6Prior Most Severe Magnetic Field Exposure
1.2.xOther
1.3CLEANLINESS LEVELS ACHIEVED
1.3.1Particulate
1.3.2Molecular
1.3.3Prohibited Materials / Processes
1.3.xOther
1.4DESIGN LIFETIME
1.4.1Probability of Success (Ps)(0 <= Ps <= 1.0)
1.4.2Operational Lifetime (for provided Ps)(years)
1.4.3On Board Expendables Lifetime(years)
1.4.4Areas of Redundancy
1.4.xOther
1.5RADIATION TOLERANCE
1.5.1Total Dose(kilorads)
1.5.2Single Event Effects System Sensitivity
1.5.xOther
1.6PAYLOAD MODEL Configuration COMPATIBILITY
1.6.1Payload (PL) Thermal Model (e.g., Format, Units, File type, etc.)
1.6.2PL Computer Aided Design Model (e.g., Format, Units, File type, etc.)
1.6.3PL Finite Element Model (e.g., Format, Units, File type, etc.)
1.6.xOther
SPACECRAFT PERFORMANCE
2.1STRUCTURAL & MECHANICAL CHARACTERISTICS
2.1.1Form Factor (e.g., 12U, 1/2 ESPA Class, ESPA Class)Adjust
2.1.2Physical Dimensions(mm)
2.1.3Primary Structure Material(s)
2.1.4System Mass, Launch Config. w/o PL, DRY(kg)
2.1.5Maximum Fuel Mass if applicable(kg)
2.1.6Maximum Payload Mass(kg)
2.1.7Coordinate System Definition (Description or Graphic)
2.1.8External Payload Envelope Dimenions (in SC coordinates)(mm)XminXmaxYminYmaxZminZmax

2.1.9 Allowable Payload CG Range (in SC coordinates) (mm) Xmin Xmax Ymin Ymax Zmin Zmax

2.1.10 Maximum Payload Moments of Inertia (MOI) (kg-m^2) Ixx Iyy Izz Ixy Ixz Izy

2.1.11Internal Payload Envelope Availability
2.1.12Maximum Payload Unobstructed Field-of-View (in SC coordiantes)(deg)XYZ-X-Y-Z

2.1.13 Maximum Payload Alignment Accuracy (in SC coordinates) (deg) X Y Z

2.1.xOther
2.2POWER AND ELECTRICAL SUBSYSTEM
2.2.1Type/Architecture
2.2.2Compatible Electrical Interfaces (RS-422, SpaceWire, etc.)
2.2.3Number of Inputs and OutputsDigital InputDigital OutputAnalog InputAnalog Output
2.2.4Ability to Accommodate Multiple Electrical Interfaces on SC
Which interfaces and how many on proven configuration?(Yes or No)
2.2.5Power Capacity Full SunWatts (W)
2.2.6Peak Payload Power (EOL)(W)
2.2.7Orbit Average Payload Power (EOL)(W)
2.2.8Allowable Payload Standy Power(W)
2.2.9Bus Voltage, Nominal Range (list regulated and unregulated)(V)
2.2.10Bus Voltage, Minimum(V)
2.2.11Bus Voltage, Maximum(V)
2.2.12Solar Array-Total Array Area(m^2)
2.2.13Solar Array-EOL Power (total)(W)
2.2.14Solar Array-BOL Power (total)(W)
2.2.15Solar Array-Cell Type and No.
2.2.16Solar Array-Articulation(axies=0,1,2,3)
2.2.17Battery-Capacity(AHr)
2.2.18Battery-Depth of Discharge(%)
2.2.19Battery-Cell Type
2.2.20Number of Batteries
2.2.21Number of Cells per Battery
2.2.22Battery-Fault Protection
2.2.23Mission Power Profile
2.2.xOther
2.3PROPULSION SUBSYSTEM
2.3.1Type/Architecture
2.3.2Propellant Type
2.3.3Pressurant Type (if applicable)
2.3.4Maximum Propellant Load(kg)
2.3.5Attitude Control Capability(Yes or No)
2.3.6Total Impulse Capability(m/sec)
2.3.xOther
2.4ATTITUDE CONTROL SUBSYSTEM
2.4.1Type/Architecture (e.g., 3 axis stabalized, spin stabilized, etc.)
2.4.2Spin Axis, if applicable(X, Y or Z)
2.4.3Orbit Knowledge(km)In TrackCross TrackAltitude

2.4.4 Pointing Accuracy (arcsec) Roll Pitch Yaw

2.4.5Pointing Stability(arcsec/sec)
2.4.6Pointing Knowledge(arcsec)RollPitchYaw
2.4.7Maximum Maneuver Rates(deg/sec)
2.4.8Pointing Stability Time Period (Following LV Separation and/or After a Maneuver)(sec)
2.4.9Pointing Constraints due to Solar Array Configuration
2.4.10Pointing Constraints for Thermal- Sun, Earth, Moon
2.4.xOther
2.5COMMAND AND DATA HANDLING SUBSYSTEM
2.5.1Type/Architecture (e.g., CCSDS formatting)
2.5.2Data Handling Capacity(kb/sec)
2.5.3Data Storage Capacity(Mb)
2.5.4Data Storage EDAC
2.5.5Selectable Data Rates(Yes or No)
2.5.6Processor Architecture/Type
2.5.7On-Board Computer CapacityProcessing Speed (MHz)RAM (KB)ROM (KB)EEPROM (KB)
2.5.xOther
2.6COMMUNICATION SUBSYSTEM
2.6.1Receive Frequency Band (X, S, UHF, etc.)
2.6.2Receiver Bandwidth
2.6.3Transmit Frequency Band (X, S, UHF, etc.)
2.6.4Transmit Bandwidth
2.6.5EIRP(W)
2.6.6G/T(dB/K)
2.6.7Type of Modulation
2.6.8Range of Modulation Index
2.6.9Coding Schemes
2.6.10Ranging (tones)(Yes or No)
2.6.112-way Doppler(Yes or No)
2.6.12Network Compatibility (STDN, DSN, TDRSS, SGLS, other)
2.6.13Spacecraft AntennaTYPE
(alphanumeric)GAIN
(numeric)PATTERNS
(alphanumeric)RANGE OF TRAVEL

(degrees)

2.6.14Telemetry Transmit Rate(kbps)
2.6.15Command Receive Rate(kbps)
2.6.16Survival/Backup Mode Link
2.6.17Number of Transmit Channels
2.6.18Subcarrier Capability on Transmitter(Yes or No)
2.6.19Transmitter Power
2.6.20Amplifier Gain
2.6.21% of Time Transmitter can be on(%)
2.6.22Ability to Accommodate Type 1 Encryption(Yes or No)
2.6.xOther
2.7THERMAL CONTROL
2.7.1Type/Architecture
2.7.2PL Interface Temperature Range(C)
2.7.xOther
2.8SOFTWARE SUBSYSTEM
2.8.1Flight Development Environment
2.8.2Flight Verification Environment
2.8.3Flight Resuse/Rework(%)
2.8.4GSE Development Environment
2.8.5GSE Verification Environment
2.8.6GSE Reuse/Rework(%)
2.8.xOther
GROUND SOLUTION PERFORMANCE
3.1DATA DISTRIBUTION
3.1.1Data Transport Network
3.1.2Support for Streaming Data
3.1.3Support for File Data
3.1.4Data Transport Protocols
3.1.5Naming Conventions
3.1.xOther
3.2GROUND SYSTEM
3.2.1Real-time
3.2.1.1What real-time engine (e.g. Neptune, RAPTOR, etc.)
3.2.1.2Virtualized?(Yes or No)
3.2.1.3Containerized?(Yes or No)
3.2.1.4Automated?(Yes or No)
3.2.1.5Initialize Hardware (e.g., FEPs and crypto)(Yes or No)
3.2.1.6Autonomously Respond to Spacecraft Telemetry(Yes or No)
3.2.1.7Estimated Coding Effort to Create New Autonomous Procedures(Yes or No)
3.2.1.8Technical Support Available?(Yes or No)
3.2.1.xOther
3.2.2Mission Planning
3.2.2.1Spacecraft Bus Maintenance Tasking(Yes or No)
3.2.2.2SC/PL Memory Management(Yes or No)
3.2.2.3Technical Support Available?(Yes or No)
3.2.2.xOther
3.2.3Flight Dynamics
3.2.3.1Attitude Maneuver (for target pointing, etc.)(Yes or No)
3.2.3.2Propulsive Maneuver (for station-keeping, momentum dumping, rendevous, etc.)(Yes or No)
3.2.3.3Orbit Determination(Yes or No)
3.2.3.4Burn Planning(Yes or No)
3.2.3.5Contact Planning(Yes or No)
3.2.3.6Sun Angle Estimation(Yes or No)
3.2.3.7Visibility (on ground and in space)(Yes or No)
3.2.3.8Scripting(Yes or No)
3.2.3.xOther
3.2.4Post-Pass Processing
3.2.4.1Report Generation(Yes or No)
3.2.4.2Out-of-Limits Telemetry Analysis(Yes or No)
3.2.4.3Trending?(Yes or No)
3.2.4.xOther
3.2.5Spectrum
3.2.5.1Ground FCC License/NTIA Certification
3.2.5.2Ground FCC License/NTIA Certification Expiration Date
3.2.5.3Ground FCC License/NTIA Radio Frequency Assignment
3.2.5.4Ground FCC License/NTIA Certification of Spectrum Supportability Control Number
3.2.5.5Space Vehicle FCC License/NTIA Certification
3.2.5.6Space Vehicle FCC License/NTIA Certification Expiration Date
3.2.5.7Space Vehicle FCC License/NTIA Radio Frequency Assignment
3.2.5.8Space Vehicle FCC License/NTIA Certification of Spectrum Supportability Control Number
3.2.5.xOther

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