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Shuttle/Agena study. Volume 1: Executive summary
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Abstract: A study to identify and define this significant space shuttle/Agena space tug interfaces is presented. The preliminary design for an Agena space tug including optional improved features is discussed. Performance capability was determined on the basis of Agena mass properties corresponding to the requirements for each of the three base line missions. A work breakdown structure in sufficient detail to assemble a complete set of cost data was developed.
Publication Date: Feb 25, 1972
Document ID:
19720013175
(Acquired Nov 22, 1995)
Accession Number: 72N20825
Subject Category: SPACE VEHICLES
Report/Patent Number: NASA-CR-115491, LMSC-D152635-VOL-1
Coverage: Final Report
Document Type: Technical Report
Publisher Information: United States
Contract/Grant/Task Num: NAS9-11949
Financial Sponsor: NASA; United States
Organization Source: Lockheed Missiles and Space Co.; Space Systems Div.; Sunnyvale, CA, United States
Description: 47p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: AGENA ROCKET VEHICLES; MANNED SPACECRAFT; SPACE TUGS; SPACECRAFT COMPONENTS; SPACECRAFT DESIGN; SPACECRAFT PROPULSION; STRAPDOWN INERTIAL GUIDANCE
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