NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Tug and payload-to-Orbiter interface requirementsThis paper presents results of a study to identify, evaluate, and develop Tug plus payload-to-Orbiter accommodation requirements. Interface areas include structural, mechanical, fluids, environmental, avionics, and safety. Each interface area was investigated to determine the best physical and operational method of accomplishing the required functions with an overriding goal of establishing sample and flexible interface requirements suitable for Tug, Tug payloads, and other cargo. The recommended system for supporting the Tug and its payload from the Orbiter employs a cylindrical load-carrying structure called a deployment adapter that has a rotational capability for Tug deployment. The design and operation of the deployment adapter and other peripheral interface equipment such as crew compartment monitor and control panels and cargo bay fluid and electrical interface panels are discussed.
Document ID
19760029832
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bock, E. H.
(General Dynamics Corp. Convair Div., San Diego, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 75-165
Report Number: AAS PAPER 75-165
Meeting Information
Meeting: Meeting on Space Shuttle Missions of the 80''s
Location: Denver, CO
Start Date: August 26, 1975
End Date: August 28, 1975
Sponsors: AAS, AIAA, IEEE, ORSA, and IMS,
Accession Number
76A12798
Funding Number(s)
CONTRACT_GRANT: NAS8-31012
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available