Nov 1984
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984spfl...26..414s&link_type=abstract
Spaceflight (ISSN 0038-6340), vol. 26, Nov. 1984, p. 414-417.
Other
Space Erectable Structures, Space Stations, Space Transportation System, Spacecraft Configurations, Orbital Assembly, Orbital Servicing, Spacecraft Design, Spacecraft Modules
Scientific paper
The configuration of the Space Station under design studies by NASA is limited only by the capabilities of the Shuttle and the purposes to which it is applied. Once the standard interlocks, launch vibration modes, and pallet designs are fixed, all other assembly of modular components, testing, and trim will be performed in space. The Station will serve for long-term experiments, as a base for planetary missions asembly, launch, and retrieval, and for loading and launching multiple satellites on an orbital transfer vehicle. Materials processing research will be carried out in the Station, as will various scientific and commercial remote sensing activities. The first operational version (1990) will require four Shuttle launches to reach an assembled mass of 70,000 kg drawing 30 kWe from solar panels and housing a crew of five. By the year 2000 the station will support 10-12 crew members in five habitat modules, will be 31 m long, will have cost $18-20 billion, and will be returning $2 billion per year. The station will be periodically reboosted to higher orbits that decay suficiently for orbiter rendezvous for supplies and assignments.
Hieatt J.
Sharples Ray
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