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Planetary/DOD entry technology flight experiments. Volume 2: Planetary entry flight experimentsThe technical feasibility of launching a high speed, earth entry vehicle from the space shuttle to advance technology for the exploration of the outer planets' atmospheres was established. Disciplines of thermodynamics, orbital mechanics, aerodynamics propulsion, structures, design, electronics and system integration focused on the goal of producing outer planet environments on a probe shaped vehicle during an earth entry. Major aspects of analysis and vehicle design studied include: planetary environments, earth entry environment capability, mission maneuvers, capabilities of shuttle upper stages, a comparison of earth entry planetary environments, experiment design and vehicle design.
Document ID
19760021156
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Christensen, H. E.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Krieger, R. J.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Mcneilly, W. R.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Vetter, H. C.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
February 29, 1976
Subject Category
Astrodynamics
Report/Patent Number
MDC-E1415-VOL-2
NASA-CR-137843
Report Number: MDC-E1415-VOL-2
Report Number: NASA-CR-137843
Accession Number
76N28244
Funding Number(s)
CONTRACT_GRANT: NAS2-8678
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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