Adaptation of sounding rocket technology to Spacelab subsatellites

Details Adaptation of sounding rocket technology to Spacelab subsatellites Adaptation of sounding rocket technology to Spacelab subsatellites

Jun 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978esasp.135..365k&link_type=abstract

In ESA European Sounding Rocket, Balloon and Related Res., with Emphasis on Expt. at High Latitudes p 365-374 (SEE N79-31637 2

Computer Science

Sound

Skylark Rocket Vehicle, Sounding Rockets, Space Transportation System, Spacelab Payloads, Design Analysis, Economic Factors, Feasibility Analysis, Get Away Specials (Sts), Low Cost

Scientific paper

A study on the adaptation of sounding rocket technology to Spacelab subsatellites was conducted. The objective of the study was to design a low cost, general purpose subsatellite of modular construction which could be adapted to various missions. The subsatellites are ejected from Spacelab and can be used to support measurement work done in conjunction with Spacelab. The target cost is discussed for the basic subsatellite. As an alternative, these subsatellites could also be flown as small self-contained payloads under the NASA Get-Away Special program.

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