System requirements (spacecraft system)

System requirements in spacecraft systems are the specific system requirements needed to design and operate a spacecraft or a spacecraft subsystem.
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Topic mentions per year

Topic mentions per year

1966-2018
02419662018

Papers overview

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2015
2015
  • JAMES F. SMOLA
  • 2015
The boom connecting the sensor platform with the Magsat spacecraft provided position and tilt adjusting capabilities for the… (More)
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2014
2014
The paper presents total ionizing dose (TID) distribution due to trapped electrons and protons at the system on module (SOM… (More)
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2012
2012
The Defense Advanced Research Projects Agency (DARPA) has recently begun an effort to further refine its Fractionated Spacecraft… (More)
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2011
2011
When the Crew Exploration Vehicle (CEV) is launched, the spacecraft adaptor (SA) fairings that cover the CEV service module (SM… (More)
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2011
2011
In order to approach the proposed attitude control process for space networking such as virtual and formation flying, a multiple… (More)
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Review
2009
Review
2009
This paper provides a survey of current state-of-the-art technologies of fractionated spacecraft, a new architecture for… (More)
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2009
2009
Fractionated spacecraft consist of physically independent, “free-flying” modules composed of various subsystems. Thus, a… (More)
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2008
2008
We deal with the attempts to measure the Lense-Thirring effect with the Satellite Laser Ranging (SLR) technique applied to the… (More)
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1998
1998
The integration of flight hardware with real-time simulations increases spacecraft attitude control systems (ACS) reliability by… (More)
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1996
1996
A key goal of NASA's New Millennium Program (NMP) is the development of technology for increasing spacecraft on-board autonomy… (More)
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