LANDSAT/MMS propulsion module design. Volume 1 : Task 4.3, trade studies
- Author:
- Mansfield, J. M.
- Published:
- Sep 24, 1976.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Etheridge, F. G. and Indrikis, J.
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary:
- Evaluations are presented of alternative LANDSAT follow-on launch configurations to derive the propulsion requirements for the multimission modular spacecraft (MMS). Two basic types were analyzed including use of conventional launch vehicles and shuttle-supported missions. It was concluded that two sizes of modular hydrazine propulsion modules would provide the most cost-effective combination for future missions of this spacecraft. Conceptual designs of the selected propulsion modules were performed to the depth permitting determination of mass properties and estimated costs.
- Other Subject(s):
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 19770008115.
Accession ID: 77N15058.
NASA-CR-144847.
SD-76-SA-0095-1-VOL-1. - Terms of Use and Reproduction:
- No Copyright.
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