Rapid_IV_DRFP_Attach_J_SC_Summary_Data_Sheet.pdf
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- Attached to
- Draft Request for Proposal - Rapid Spacecraft Acquisition IV Federal contract opportunity
- Solicitation number
- 80GSFC19R0016
About this file
This document provides details for the Draft Request for Proposal for the Rapid Spacecraft Acquisition IV contract opportunity. The National Aeronautics and Space Administration Goddard Space Flight Center plans to issue this RFP to acquire spacecraft and related services through multiple-award, firm fixed price, indefinite delivery indefinite quantity contracts. The scope of work involves efforts from receipt of a delivery order through spacecraft development, launch, and on-orbit acceptance. The contracts would have a base period of five years and one five-year option period, not to exceed $6 billion total. Eligible offerors must have led two successful spacecraft developments and designs with a minimum 7-kilogram payload mass and 20-watt payload power capability. The anticipated RFP release dates are mid-to-late April for the draft and June 2019 for the final. Questions must be submitted in writing by the draft RFP deadline.
Attach J - SC Summary Data Sheet
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Text version
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)
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
File details come from the government source that posted it. Updated .