Optimization of low-perigee spacecraft aerodynamics
Author:
Affiliation:
1. Maryland, Univ., College Park
2. NASA, Goddard Space Flight Center, Greenbelt, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-549
Reference30 articles.
1. Rocketborne Rayleigh lidar for in situ measurements of neutral atmospheric density
2. Diurnal density variations measured by the San Marco 3 satellite in the equatorial atmosphere
3. Exospheric temperature inferred from the Aeros-A neutral composition measurement
4. Empirical model of global thermospheric temperature and composition based on data from the Ogo 6 quadrupole mass spectrometer
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1. Reentry Envelope Determination Part II: Structural Failure Due To Atmospheric Heating;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2006-06-25
2. Stability of Flexible Spacecraft During a Shallow Aeroassist;Journal of Spacecraft and Rockets;2005-03
3. Optimization of Low-Perigee Spacecraft Aerodynamics;Journal of Spacecraft and Rockets;2003-01
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