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100   $a20111113j196810    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEntries from earth orbit that simulate acceleration stresses of manned planetary missions /$fby Frederick G. Edwards
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dOctober 1968.
215   $a1 online resource (32 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4847
300   $a"October 1968."
320   $aIncludes bibliographical references (page 32).
606   $aAcceleration (Mechanics)
606   $aInterplanetary voyages
606   $aSpace vehicles$xAtmospheric entry
606   $aWeightlessness
606   $aAcceleration (Mechanics)$2fast
606   $aInterplanetary voyages$2fast
606   $aSpace vehicles$xAtmospheric entry$2fast
606   $aWeightlessness$2fast
615  0$aAcceleration (Mechanics)
615  0$aInterplanetary voyages.
615  0$aSpace vehicles$xAtmospheric entry.
615  0$aWeightlessness.
615  7$aAcceleration (Mechanics)
615  7$aInterplanetary voyages.
615  7$aSpace vehicles$xAtmospheric entry.
615  7$aWeightlessness.
700   $aEdwards$b Frederick G.$01419940
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aAmes Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910714070103321
996   $aEntries from earth orbit that simulate acceleration stresses of manned planetary missions$93536060
997   $aUNINA