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ID No : 552   Edit
Title: Regolith-Derived Heat Shield for Planetary Body Entry and Descent System with In Situ Fabrication
Summary / Review : Abstract: "In this paper we will discuss a new mass-efficient and innovative way of protecting high-mass spacecraft during planetary Entry, Descent & Landing (EDL). Heat shields fabricated in situ can provide a thermal-protection system (TPS) for spacecraft that routinely enter a planetary atmosphere. By fabricating the heat shield with space resources from regolith materials available on moons and asteroids, it is possible to avoid launching the heat-shield mass from Earth. Three regolith processing and manufacturing methods will be discussed: 1) oxygen & metal extraction ISRU processes produce glassy melts enriched in alumina and titania, processed to obtain variable density, high melting point and heat-resistance; 2) compression and sintering of the regolith yield low density materials; 3) in-situ derived high-temperature polymers are created to bind regolith particles together, with a lower energy budget."

Meeting Information: Earth and Space 2012/ASCE; NIAC Fellows Meeting; FROM; 15-18 Apr. 2012; 16-17 Nov. 2011; Pasadena, CA; Arlington, VA; United States

Subject Terms: ALUMINUM OXIDES; ATMOSPHERIC ENTRY; EXTRATERRESTRIAL RESOURCES; FABRICATION; HEAT SHIELDING; IN SITU RESOURCE UTILIZATION; REGOLITH; SPACE LOGISTICS; SPACECRAFT DESIGN; THERMAL PROTECTION; THERMAL RESISTANCE; TITANIA; WEIGHT REDUCTION
Author(s) : Hogue, Michael D., [Electrostatics & Surface Physics Laboratory, NASA, Kennedy Space Center, FL ]
Mueller, Robert P., [Surface Systems Office, NASA, Kennedy Space Center, FL]
Rasky, Daniel, [Emerging Space Office, NASA, Ames Research Center]
Hintze, Paul, [Corrosion Laboratory, NASA, Kennedy Space Center, FL]
Sibille, Laurent, [QNA ESC, Kennedy Space Center, FL]
Publication Type : Paper within a Parent compilation, or Presentation at a Professional conference
Publication Date: 2011
Pages : 13
# of References : 21
Copyright By : Public domain
Category(s) : Bases, industry and manufacturing / Resource processing and outputs / Glasses, fiberglass, and ceramics
Bases, industry and manufacturing / Resource processing and outputs / Refractories
Bases, industry and manufacturing / Resource processing and outputs / Sintering
Products
Transportation / Aerobraking
Progress Type: A,T ( A=Analysis only, D=Design, T=Testing, C=Completed or Commercial product )
Web URL : http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110016723_2011017765.pdf
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NTRS : 20110016723
Other Ref # : KSC-2011-268, KSC-2011-268RR, KSC-2011-268R
Submitted by : MEP
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