LEADER 01658nam  2200493Ia 450 
001 9910697260903321
005 20230902161558.0
035   $a(CKB)5470000002386312
035   $a(OCoLC)646196418
035   $a(EXLCZ)995470000002386312
100   $a20100707d1994      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aMethod for molding structural parts utilizing modified silicone rubber$b[electronic resource]
205   $a[Redacted ed.]
210  1$a[Washington, DC] :$c[National Aeronautics and Space Administration],$d[1994]
215   $a1 online resource $cillustrations
225 1 $aNASA case ;$vno. LAR 15217-1
300   $aTitle from PDF title screen (NASA, viewed July 6, 2010).
410  0$aNASA case ;$vLAR-15217-1.
606   $aMolding materials$2nasat
606   $aPreforms$2nasat
606   $aSilicone rubber$2nasat
606   $aTemperature effects$2nasat
606   $aThermal expansion$2nasat
606   $aMaterials$xEffect of temperature on
606   $aExpansion (Heat)
615  7$aMolding materials.
615  7$aPreforms.
615  7$aSilicone rubber.
615  7$aTemperature effects.
615  7$aThermal expansion.
615  0$aMaterials$xEffect of temperature on.
615  0$aExpansion (Heat)
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697260903321
996   $aMethod for molding structural parts utilizing modified silicone rubber$93101003
997   $aUNINA