Session

Session VII: Launch Systems and Orbital Manuvering

Abstract

The launch problem for small payloads is nowhere as serious as it is for scientific and academic users, who cannot tap the purchasing power available to spacecraft funded by the military and large corporations. The options available for the researcher at a university who has an instrument or a spacecraft are limited, sometimes depressingly so. Dedicated vehicles are usually unaffordable, and secondary payload opportunities require meeting a host of requirements, from payload design to timing to integration, dependent on the needs of the primary payload. In this paper, the authors survey the options available and answer the question, “Where do I start?” Sources of potential rides, including NASA, military, commercial, and non-U.S. programs and organizations were surveyed. The results are presented here, along with recommendations for an improved process which, at low cost, could improve the “matchmaking” system and simplify the obstacle course faced by spacecraft and instrument developers today.

Share

COinS
 
Aug 14th, 3:15 PM

“Where Do I Start?” Rides to Space for Scientific and Academic Payloads

The launch problem for small payloads is nowhere as serious as it is for scientific and academic users, who cannot tap the purchasing power available to spacecraft funded by the military and large corporations. The options available for the researcher at a university who has an instrument or a spacecraft are limited, sometimes depressingly so. Dedicated vehicles are usually unaffordable, and secondary payload opportunities require meeting a host of requirements, from payload design to timing to integration, dependent on the needs of the primary payload. In this paper, the authors survey the options available and answer the question, “Where do I start?” Sources of potential rides, including NASA, military, commercial, and non-U.S. programs and organizations were surveyed. The results are presented here, along with recommendations for an improved process which, at low cost, could improve the “matchmaking” system and simplify the obstacle course faced by spacecraft and instrument developers today.