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Hypersonic Inflatable Aerodynamic Decelerator Ground Test DevelopmentHypersonic Inflatable Aerodynamic Decelerator (HIAD) technology readiness levels have been incrementally matured by NASA over the last thirteen years, with most recent support from NASA's Space Technology Mission Directorate (STMD) Game Changing Development Program (GCDP). Recently STMD GCDP has authorized funding and support through fiscal year 2015 (FY15) for continued HIAD ground developments which support a Mars Entry, Descent, and Landing (EDL) study. The Mars study will assess the viability of various EDL architectures to enable a Mars human architecture pathfinder mission planned for mid-2020. At its conclusion in November 2014, NASA's first HIAD ground development effort had demonstrated success with fabricating a 50 W/cm2 modular thermal protection system, a 400 C capable inflatable structure, a 10-meter scale aeroshell manufacturing capability, together with calibrated thermal and structural models. Despite the unquestionable success of the first HIAD ground development effort, it was recognized that additional investment was needed in order to realize the full potential of the HIAD technology capability to enable future flight opportunities. The second HIAD ground development effort will focus on extending performance capability in key technology areas that include thermal protection system, lifting-body structures, inflation systems, flight control, stage transitions, and 15-meter aeroshell scalability. This paper presents an overview of the accomplishments under the baseline HIAD development effort and current plans for a follow-on development effort focused on extending those critical technologies needed to enable a Mars Pathfinder mission.
Document ID
20160006468
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Del Corso, Jospeh A.
(NASA Langley Research Center Hampton, VA, United States)
Hughes, Stephen
(NASA Langley Research Center Hampton, VA, United States)
Cheatwood, Neil
(NASA Langley Research Center Hampton, VA, United States)
Johnson, Keith
(NASA Langley Research Center Hampton, VA, United States)
Calomino, Anthony
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 20, 2016
Publication Date
June 15, 2015
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-21355
Meeting Information
Meeting: International Planetary Probe Workshop (IPPW-12)
Location: Cologne
Country: Germany
Start Date: June 15, 2015
End Date: June 19, 2015
Sponsors: Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
Funding Number(s)
WBS: WBS 630154.01.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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