RIV RFP Attach J_SC Summary Data Sheet.pdf
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- Attached to
- Request for Proposals (RFP) for the Rapid Spacecraft Acquisition IV (Rapid IV) On-Ramp I
- Solicitation number
- 80GSFC19R0016
About this file
This request for proposals solicits spacecraft designs and related services to support NASA and other federal agencies through indefinite delivery, indefinite quantity contracts with multiple awardees. Offerors must propose flight-proven spacecraft designs ranging from 7kg payload mass and 20W payload power minimums to larger designs. Proposals are due January 10, 2020 with contracts to have a 10-year ordering period from award. Evaluation will assess ten technical standards including two successful past spacecraft developments. The North American Industry Classification code is 336414 and small businesses must have 1,250 employees or fewer. Firm fixed price delivery orders will be issued against the contracts which may involve work at contractor or government facilities.
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SAMPLE (Delete this column from submitted form)
Venture Satellite Corporation
Company Name Company Name Company Name 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
Compatibilty 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) 36
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.
Rapid IV - Spacecraft Summary Data Sheet - Attachment J
Sheet1
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