Space vehicle propulsion systems - Environmental space hazardsAn evaluation of hazards which exist in geo-lunar space and have the potential to negatively affect a long-term mission-oriented spacecraft systems is presented based on published data. The hazards are categorized as pervasive (radiation), incident specific (meteoroids and thermal shock), and chemically corrosive (monatomic oxygen). It appears that the number one priority should be the development of new materials; and the secondary concern should be the development of fabrication techniques for the exterior hull, so that incident specific hazards can be minimized in an active fashion. The pervasive hazard can be dealt with by exploring on-board circuit technology with ancillary monitoring systems. Effects of thermal shock on the exterior nozzle, directional gimbals, and internal combustion chamber geometry seem to need more investigation.
Document ID
19900053490
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bahr, G. K. (Cincinnati Univ. OH, United States)
Disimile, P. J. (Cincinnati, University OH, United States)