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Planetary/DOD entry technology flight experiments. Volume 1: Executive summaryThe feasibility of using the space shuttle to launch planetary and DoD entry flight experiments was examined. The results of the program are presented in two parts: (1) simulating outer planet environments during an earth entry test, the prediction of Jovian and earth radiative heating dominated environments, mission strategy, booster performance and entry vehicle design, and (2) the DoD entry test needs for the 1980's, the use of the space shuttle to meet these DoD test needs, modifications of test procedures as pertaining to the space shuttle, modifications to the space shuttle to accommodate DoD test missions and the unique capabilities of the space shuttle. The major findings of this program are summarized.
Document ID
19760021155
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
NASA-CR-137842
MDC-E1415-VOL-1
Report Number: NASA-CR-137842
Report Number: MDC-E1415-VOL-1
Accession Number
76N28243
Funding Number(s)
CONTRACT_GRANT: NAS2-8678
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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