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The Space Tug mission role and program planning.More than half of the planned payload programs require a velocity increment beyond that nominally provided by the Space Shuttle. The reusable Space Tug system can satisfy this placement requirement and, in addition, can provide other, vital operational services for payloads in the 1980s. To realize maximum operational and economic benefits, it is desired that an orbital propulsive stage such as the Space Tug be available concurrently with Space Shuttle initial operations. Potential tug missions, significant interfaces, system characteristics, and configuration alternatives are discussed in conjunction with salient program planning factors.
Document ID
19730051286
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schnyer, A. D.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 73-609
Meeting Information
Meeting: Joint Space Mission Planning and Execution Meeting
Location: Denver, CO
Start Date: July 10, 1973
End Date: July 12, 1973
Sponsors: AIAA, ASME, SAE
Accession Number
73A36088
Distribution Limits
Public
Copyright
Other

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