The air force/ultramet solar-thermal receiver/absorber propulsion (STRAP) device

Details The air force/ultramet solar-thermal receiver/absorber propulsion (STRAP) device The air force/ultramet solar-thermal receiver/absorber propulsion (STRAP) device

Jan 1997

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1997aipc..387..499f&link_type=abstract

Space technology and applications international forum (STAIF - 97). AIP Conference Proceedings, Volume 387, pp. 499-504 (1997).

Computer Science

Performance

Energy Storage Systems, Including Capacitor Banks, Performance Characteristics Of Energy Conversion Systems, Figure Of Merit

Scientific paper

A rhenium solar-thermal receiver/absorber propulsion (STRAP) device has been designed and fabricated. Its uniqueness lies in its simplicity of design and fabrication, consisting of just three components electron beam welded together: a rhenium foam heat exchanger between inner and outer rhenium structural shells, with the thrust chamber integral to the outer shell. Plans have been developed for testing this device at the Air Force Phillips Laboratory.

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