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Comparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel / / M.H. Lucy and R.D. Buehrle, J.P. Woolley
Comparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel / / M.H. Lucy and R.D. Buehrle, J.P. Woolley
Autore Lucy M. H.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1996
Descrizione fisica 1 online resource (i, 50 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Spacecraft design
Booster rocket engines
Actuators
Shock spectra
Stage separation
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707239603321
Lucy M. H.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Design and verification guidelines for vibroacoustic and transient environments [[electronic resource]]
Design and verification guidelines for vibroacoustic and transient environments [[electronic resource]]
Pubbl/distr/stampa [Marshall Space Flight Center, Ala.] : , : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, Component Analysis Branch, Systems Dynamics Laboratory, , [1986]
Descrizione fisica iv, 23 pages : digital, PDF file
Collana NASA technical memorandum
Soggetto topico Acoustic measurement
Design analysis
Proving
Random vibration
Shock spectra
Structural vibration
Transient response
Vibration tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697712003321
[Marshall Space Flight Center, Ala.] : , : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, Component Analysis Branch, Systems Dynamics Laboratory, , [1986]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui