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Mariner 9 propulsion subsystem performance during interplanetary cruise and Mars orbit insertionOn 14 November 1971 the Mariner 9 1334-N-(300-lbf)-thrust rocket engine was fired for just over 15 min to place the first man-made satellite into orbit about Mars. Propulsion subsystem data gathered during the 5-month interplanetary cruise and orbit insertion are of significance to future missions of this type. Specific results related to performance predictability, zero g heat transfer, and nitrogen permeation, diffusion, and solubility values are presented.
Document ID
19720021302
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cork, M. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
French, R. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Leising, C. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Schmit, D. D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Publication Information
Publication: JPL Quarterly Tech. Rev., Vol. 2, No. 1
Subject Category
Propulsion Systems
Accession Number
72N28952
Distribution Limits
Public
Copyright
Public Use Permitted.
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