01907oam 2200517I 450 991070723960332120160621154007.0(CKB)5470000002463113(OCoLC)227848727(EXLCZ)99547000000246311320080512j199612 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierComparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel /M.H. Lucy and R.D. Buehrle, J.P. WoolleyHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 1996.1 online resource (i, 50 pages)illustrationsNASA technical memorandum ;110257Title from title screen (viewed June 20, 2016)."December 1996.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Spacecraft designnasatBooster rocket enginesnasatActuatorsnasatShock spectranasatStage separationnasatSpacecraft design.Booster rocket engines.Actuators.Shock spectra.Stage separation.Lucy M. H.1387210Buehrle Ralph D(Ralph David),Woolley J. P.Langley Research Center,United States.National Aeronautics and Space Administration,DTICEDTICEOCLCQGPOBOOK9910707239603321Comparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel3436789UNINA