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Enabling Future Low-Cost Small Mission ConceptsA SmallSat using a small Radioisotope Power System for deep space destinations could potentially fit into a Discovery class mission cost cap and perform significant science with a timely return of data. Only applicable when the Discovery 12 guidelines were applied. Commonality of hardware and science instruments among identical spacecraft enabled to meet the Discovery Class mission cost cap. Multiple spacecraft shared the costs of the Launch Approval Engineering Process. Assumed a secondary science instrument was contributed. Small RPS could provide small spacecraft with a relatively high power (approx. 60 We) option for missions to deep space destinations (> 10 AU) with multiple science instruments. Study of Centaur mission demonstrated the ability to achieve New Frontiers level science. Multiple spacecraft possible with small RPS, allowing for multiple targets, science from multiple platforms, and/or redundancy.
Document ID
20160009676
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
Authors
Lee, Young
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bairstow, Brian
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Amini, Rashied
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Zakrajsek, June
(NASA Glenn Research Center Cleveland, OH, United States)
Oleson, Steven
(NASA Glenn Research Center Cleveland, OH, United States)
Cataldo, Robert
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2016
Publication Date
May 5, 2014
Subject Category
Spacecraft Design, Testing And Performance
Space Sciences (General)
Meeting Information
Meeting: AIAA SpaceOps 2014 International Conference on Space Operations
Location: Pasadena, CA
Country: United States
Start Date: May 5, 2014
End Date: May 9, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other

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