Deployable multi-payload platformMany space payloads with similar mission requirements can be grouped and accommodated on an orbiting platform which provides high-capacity, centralized services. Various concepts for such a platform were devised and evaluated to identify optimal features, interface prospects and areas of technological challenge. Guidelines included minimum and augmented mission models for science and applications payloads for the 1985-90 time period, minimum extension of the Orbiter capability, maximum use of the Orbiter remote manipulator system and capitalization on EVA where applicable. Deployable structures were employed to provide spacious payload berthing on a platform which can be highly-compacted for shuttle delivery.
Document ID
19790050735
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Jenkins, L. M. (NASA Johnson Space Center Spacecraft Design Div., Houston, Tex., United States)
Runge, F. C. (McDonnell Douglas Astronautics Co. Huntington Beach, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 79-0928Report Number: AIAA PAPER 79-0928
Meeting Information
Meeting: Conference on Advanced Technology for Future Space Systems