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Technology Overview and Assessment for Small-Scale EDL SystemsMotivated by missions to land large rovers and humans at Mars and other bodies, high-mass EDL technologies are a prevalent trend in the research community. In contrast, EDL systems for low-mass payloads have attracted less attention. Significant potential in science and discovery exists in small-scale EDL systems. Payloads acting secondary to a flagship mission are a currently under-utilzed resource. Before taking advantage of these opportunities, further developed of scaled EDL technologies is required. The key limitations identified in this study are compact decelerators and deformable impact systems. Current technologies may enable rough landing of small payloads, with moderate restrictions in packaging volume. Utilization of passive descent and landing stages will greatly increase the applicability of small systems, allowing for vehicles robust to entry environment uncertainties. These architectures will provide an efficient means of achieving science and support objectives while reducing cost and risk margins of a parent mission.
Document ID
20160012770
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Heidrich, Casey R.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Smith, Brandon P.
(NASA Ames Research Center Moffett Field, CA United States)
Braun, Robert D.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
October 31, 2016
Publication Date
June 13, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN32700
Report Number: ARC-E-DAA-TN32700
Meeting Information
Meeting: International Planetary Probe Workshop
Location: Laurel, MD
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: Johns Hopkins Univ., NASA Headquarters
Funding Number(s)
CONTRACT_GRANT: NNX15AQ28H
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
small spacecraft
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