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Site alteration effects from rocket exhaust impingment during a simulated Viking Mars landing. Part 1, Nozzle development and physical site alternation
Content Provider | HathiTrust Digital Library |
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Author | Romine, G. L Gliozzi, J Reisert, T. D |
Editor | G.L. Romine J. Gliozzi T.D. Reisert |
Organization | Martin Marietta Corporation. |
Description | Prepared by Martin Marietta Corporation, Denver Division, Denver, Colo. for Langley Research Center NAS1-9000 815-20-00-00-00 |
Volume Number | NASA CR-2252 |
Language | English |
Publisher | National Aeronautics and Space Administration |
Publisher Date | 1973-01-01 |
Publisher Place | Springfield Washington D.C. |
Access Restriction | Open |
Rights License | Items in this record are available as Public Domain, Google-digitized. View the access and use profile at http://www.hathitrust.org/access_use#pd-google. Please see individual items for rights and use statements |
Subject Keyword | Viking 1975 entry vehicle Soft landing Mars surface Mars landing Landing sites Rocket exhaust Propulsion system configurations Jet impingement Exhaust gases |
Content Type | Text |
Resource Type | Book |