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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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PERMANENT code(s) : | L,U |
(Explanation of the last 3 rows above) |
In the row above, there are up to 4 possibilities: U = URL you can click on to get a copy instantly from another source on the internet, or request it from that source D = Downloadable from PERMANENT (such as because no other URL known...) L = LAN copy, PERMANENT has a digital copy but not downloadable from our website P = Paper copy in the PERMANENT office Typically, only 0 to 3 methods are available. |
NTRS : | 20110016723 |
Other Ref # : | KSC-2011-268, KSC-2011-268RR, KSC-2011-268R |
Submitted by : | MEP |
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