Paper
23 October 1984 Co-Orbiting Platform And Services To Optics Payloads
Kenneth H. Rourke
Author Affiliations +
Proceedings Volume 0493, Optical Platforms; (1984) https://doi.org/10.1117/12.943802
Event: The National Symposium and Workshop on Optical Platforms, 1984, Huntsville, United States
Abstract
The Co-Orbiting Platform is a major element in NASA's new initiative to develop and deploy a permanent space station in the early 1990's. This separate, unmanned free flying space platform supports a variety of space payloads with standard orbital services including: mechanical attachment, pointing control, electrical power, thermal control and data communications. It enhances the overall space station architecture by offering the more controlled space environments and additional mission flexibility supplied by unmanned free flying vehicles. The co-orbiting space platform additionally offers the servicing and transportation economy made possible by the nearby space station. This paper reviews the general features of space platforms drawing on previous space platform and space station studies conducted by NASA. Co-orbital characteristics and operations are reviewed. Plat-form services, particularly those pertinent to optics payloads are discussed; these include viewing access; pointing stability and control; contamination environmental control; electrical power services; thermal control; and data handling, storage and two-way communications.
© (1984) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Kenneth H. Rourke "Co-Orbiting Platform And Services To Optics Payloads", Proc. SPIE 0493, Optical Platforms, (23 October 1984); https://doi.org/10.1117/12.943802
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Space telescopes

Space operations

Data communications

Surface plasmons

Contamination

Aerospace engineering

Interfaces

Back to Top