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 75-165Report Number: AAS PAPER 75-165
Meeting Information
Meeting: Meeting on Space Shuttle Missions of the 80''s