RIV RFP Attach J_SC Summary Data Sheet.pdf
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- Attached to
- REQUEST FOR PROPOSAL (RFP) - FOR THE RAPID SPACECRAFT ACQUISITION IV (RAPID IV) ON-RAMP III Federal contract opportunity
- Solicitation number
- 80GSFC19R0016-Rev4
About this file
This document contains a spacecraft summary data sheet template and details of a federal contract opportunity for the Rapid Spacecraft Acquisition IV (Rapid IV) On-Ramp III solicitation. The data sheet template requests key specifications for prospective spacecraft, including payload power and mass capacity, bus characteristics, orbital parameters, propulsion capabilities, program schedule, and optional enhancement packages. The related solicitation is issued by NASA's Goddard Space Flight Center to acquire rapid, low-cost spacecraft for science and technology demonstrations. Responses are due based on the issuance date of the one-time Determination of Capability, with spacecraft ready for payload integration and testing within 24 months of award and launch no more than 36 months later.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Rapid IV RFP Questions and Answers.pdf | ||
| RIV RFP Attach B.pdf | ||
| RIV RFP Attach E.pdf | ||
| RIV RFP Attach K_Core Sys Perform Charact Subsys Details .pdf | ||
| RIV RFP 80GSFC19R0016-SF30_pgs 2-40_Final.pdf | ||
| RIV RFP SF33 for OR3.pdf | ||
| RIV RFP (Sections B-M) Rev4 _Final.pdf | ||
| RIV RFP Section L_Enclosure 2_IT Security Mgmt Plan.pdf | ||
| RIV RFP Attach D_Project Control Plan.pdf | ||
| RIV RFP Attach F_IT Security Applic Docs List-Rev1.pdf | ||
| RIV OR3 RFP Cover Ltr_Final.pdf | ||
| RIV RFP 80GSFC19R0016-SF30 Amend 4.pdf | ||
| RIV RFP Section L-Exhibit 1 -SC Verifi Quest Rv2.pdf | ||
| RIV RFP CDRL1 Enclosure 1.pdf | ||
| RIV RFP Attach A_SOW.pdf | ||
| RIV RFP Attach C_CDRL.pdf | ||
| RIV RFP Section-L-Enclosure 1.pdf | ||
| RIV RFP Attach H_Rev 2.pdf | ||
| RIV RFP Attach I.pdf |
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Text version
RAPID IV RFP #80GSFC19R0016 Rev 4 CONTRACT #TBD
ATTACHMENT J
RAPID IV
RFP
SPACECRAFT SUMMARY DATA
SHEET
Date TBD
(TO BE SUBMITTED UPON ISSUANCE OF THE ONE-TIME DO)
Rapid IV - Spacecraft Summary Data Sheet - Attachment J
SAMPLE (Delete this column from submitted form)
Compatibilty
Venture Satellite Corporation
Company Name
Units SuperSat-1 Core S/C 1 name Core S/C 2 name Core S/C 3 name Core S/C N name
Orbit Average Payload Power (EOL) W (EOL) 100
Maximum Payload Mass kg 100
Bus Dry mass (w/o Payload) kg 150
Science Data Downlink kbps 1000
Science Data Storage (Capacity) Mbit 256
Pointing Knowledge arcsec 360
Pointing Control arcsec 3600
Pointing Stability (Jitter) arcsec/sec 10
Slewrate deg/min n/a
Mission Design Life years 2
Compatible LVs (names) Delta II, Pegasus
Nominal Orbit Altitude, Inclination, Type, Other 500 km, 98 deg, Sun
Synch
Types of Orbits Available as needed LEO from 28.5 to 98 deg, up to 1000km
External Payload Volume meters 1m dia x 1.5 m h
Internal Payload Volume meters 2 bays, .4 & .2 m3
Description ACS type spinner, 3-axis, etc.
Star Trackers # of STs 2
GPS # recievers 1
Batteries cell type/capacity (Ah)
NiCd/20 Ah
Solar Arrays cell type/Area (m)
Single Junction GaAs, .5m2
Main Bus Voltage Range volts 28-34
C&DH Bus Architecture description 1553
Downlink Formats CCSDS, STDN, etc STDN
Comm Up\Downlink Band
S, X, UHF, Ka, Ku, etc. S-band
Structure description
Al Honeycomb Hexagon
Propulsion type, fuel Mono-prop (N2H4)
Propellant Capacity kg 50
Max delta V m/s 5
Programmatic & Other heritage mission(s) name(s) SuperSat, CometSat nominal schedule months (ATP to ready for payload I&T) nominal schedule months
(ATP to launch)
Option Name
Options Contract Option #1
Enhanced Data Storage
Contract Option #2
Power Upgrade Package
Contract Option #3
Ground Operations
Center
Contract Option #N etc.
| ATTACHMENT J |
| Date TBD |
| (TO BE SUBMITTED UPON ISSUANCE OF THE ONE-TIME DO) |
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