NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Mars Orbiter Study. Volume 1: SummarySpacecraft system and subsystem designs were developed at the conceptual level to perform either of two Mars orbiter missions, a climatology mission and an aeronomy mission. The HS 376 spacecraft is the basis for the design because it has the lowest cost due to its production line status. The mission design, science instrument accommodation, and spacecraft design are summarized.
Document ID
19830010567
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Drean, R.
(Hughes Aircraft Co. El Segundo, CA, United States)
Macpherson, D.
(Hughes Aircraft Co. El Segundo, CA, United States)
Steffy, D.
(Hughes Aircraft Co. El Segundo, CA, United States)
Vargas, T.
(Hughes Aircraft Co. El Segundo, CA, United States)
Shuman, B.
(Hughes Aircraft Co. El Segundo, CA, United States)
Anderson, K.
(Hughes Aircraft Co. El Segundo, CA, United States)
Richards, B.
(Hughes Aircraft Co. El Segundo, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-166428
REPT-82(44)00361/F1886-VOL-1
NAS 1.26:166428
Report Number: NASA-CR-166428
Report Number: REPT-82(44)00361/F1886-VOL-1
Report Number: NAS 1.26:166428
Accession Number
83N18838
Funding Number(s)
PROJECT: RTOP 186-30-20-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available