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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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Requirements analysisRequirements engineeringRequirements managementStatement of work
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Systems engineering

Papers overview

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2018
2018
DIRECT MULTIPIXEL IMAGING AND SPECTROSCOPY OF AN EXOPLANET WITH A SOLAR GRAVITY LENS MISSION NASA Innovative Advanced Concepts (NIAC) Phase I FINAL REPORT
Slava G. Turyshev1, Michael Shao1, Leon Alkalai1, Nitin Aurora1, Darren Garber3, Henry Helvajian2, Tom Heinsheimer2, Siegfried… Expand
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2017
2017
Assessment of Multimode Spacecraft Micropropulsion Systems
Multimode spacecraft micropropulsion systems that include a high-thrust chemical mode and high-specific impulse electric mode are… Expand
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2016
2016
Magnetic shield design modeling and validation for SWOT spacecraft Ka-band Extended Interaction Klystron
Two Extended Interaction Klystrons (EIKs) containing strong permanent magnets were modeled magnetically in a representative… Expand
2012
2012
Evaluating a Fractionated Spacecraft system: A business case tool for DARPA's F6 program
The Defense Advanced Research Projects Agency (DARPA) has recently begun an effort to further refine its Fractionated Spacecraft… Expand
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Highly Cited
2010
Highly Cited
2010
Relativistic electron loss due to ultralow frequency waves and enhanced outward radial diffusion
[1] Using the THEMIS and GOES satellites and ground-based magnetometers, the loss of outer zone radiation belt electrons through… Expand
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2009
2009
FRACTIONATED SPACE ARCHITECTURES: TRACING THE PATH TO REALITY
In an effort to achieve responsiveness, increase effectiveness, and reduce the uncertainty involved in maintaining a space… Expand
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Highly Cited
2008
Highly Cited
2008
The characteristics and consequences of the break-up of the Fengyun-1C spacecraft
Abstract The intentional break-up of the Fengyun-1C spacecraft on 11 January 2007 via a hypervelocity collision with a ballistic… Expand
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2001
2001
Analysis of a Magnetic Three-Axis Stabilized Attitude Control System for the NPSAT1 Spacecraft
Abstract : The NPSAT1 satellite uses an active magnetic torque rod system, with a magnetometer for attitude determination, to… Expand
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1998
1998
Real-time spacecraft simulation and hardware-in-the-loop testing
  • Alan Ptak, K. Foundy
  • Proceedings. Fourth IEEE Real-Time Technology and…
  • 1998
    • Corpus ID: 31446821
The integration of flight hardware with real-time simulations increases spacecraft attitude control systems (ACS) reliability by… Expand
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Highly Cited
1982
Highly Cited
1982
An update on the Active Magnetospheric Particle Tracer Explorers (AMPTE) program
The principles involved in the AMPTE mission's active experiments are discussed together with the role of the AMPTE satellites… Expand
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