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101 0 $aeng
200 1 $aFinite fields and applications$eProceedings of the third International Conference, Glasgow, July 1995$fedited by S. Cohen, H. Niederreiter
210   $aCambridge$cCambridge University Press$dc1996
215   $axx, 401 p.$d23 cm
225 1 $aLondon Mathematical Society lecture note series$v233
610 0 $aGeometria combinatoria$aCongressi
676   $a512.3
700  1$aFinite$0492450
702  1$aCohen,$bS.
702  1$aNiederreiter,$bHarald
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100   $a20150107j201309    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDevelopment of the Orion crew-service module umbilical retention and release mechanism /$fDamon Delap, Joel Glidden and Christopher Lamoreaux
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dSeptember 2013.
215   $a1 online resource (9 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2013-216583
300   $aTitle from title screen (viewed Jan. 7, 2015).
300   $a"September 2013."
300   $a"Prepared for the 15th European Space Mechanism and Tribology Symposium sponsored by the European Space Agency, Noordwijk, The Netherlands, September 25-27, 2013."
320   $aIncludes bibliographical reference (page 9).
606   $aCommand service modules$2nasat
606   $aAerodynamic loads$2nasat
606   $aFault tolerance$2nasat
606   $aFlight tests$2nasat
606   $aLife support systems$2nasat
606   $aSpacecraft modules$2nasat
615  7$aCommand service modules.
615  7$aAerodynamic loads.
615  7$aFault tolerance.
615  7$aFlight tests.
615  7$aLife support systems.
615  7$aSpacecraft modules.
700   $aDelap$b Damon$01396804
702   $aGlidden$b Joel
702   $aLamoreaux$b Christopher
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702782903321
996   $aDevelopment of the Orion crew-service module umbilical retention and release mechanism$93457498
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