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Risk analysis of earth return options for the Mars Rover/sample return mission [microform].
Text
Webster, Tex. : Eagle Engineering, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Self-adaptive difference method for the effective solution of computationally complex problems of boundary layer theory [microform] / W. Schönauer ... [et al.].
Text
Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Rarefied gas effects on aerobraking/reentry vehicles with wakes [microform] / prepared by Amolak C. Jain.
Text
[Huntsville, AL] : Remtech ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A vehicle health monitoring system for the space shuttle reaction control system during reentry [microform] / by Anthony David Rosello.
Text
Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Orbiter rarefied-flow reentry measurements from the OARE on STS-62 [microform] / R.C. Blanchard, J.Y. Nicholson.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Convective and radiative heating for vehicle return from the Moon and Mars [microform] / R.B. Greendyke, P.A. Gnoffo.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Development of the reentry flight dynamics simulator for evaluation of Space Shuttle Orbiter entry systems / Lawrence F. Rowell, Richard W. Powell, and Howard W. Stone, Jr.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980.
1980-10
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70979Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / Parviz A. Bahrami.
Text
Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 2012.
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo37271No results found from Digital Research Books Beta
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