Hazards associated with a LEM abort near the lunar surface
Propellant explosion hazard in lunar module abort descent near lunar surface
Teixeira, C.↗
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Results for “EXPLOSIVE”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Nondestructive testing of Apollo CSM spacecraft ordnance devices by neutron radiography
Nondestructive testing of Apollo CSM /Command and Service Module/ spacecraft ordnance explosive devices by indirect and direct neutron radiography
Ewbank, N. M.↗
Supernovae, neutron stars, and pulsars
Pulsars pulse duration and shape as key to neutron stars linkage with supernova explosions
Cameron, A. G. W.↗
Weak shock waves in turbulent media
Weak shock thicknesses with turbulent scattering as dissipative mechanism compared with magnitude in sonic boom flight tests and explosions
George, A. R.↗
Static and dynamic origin of kink bands in micas
Static and shock kink bands in biotite deformed by metamorphism, meteorite impact, nuclear explosion and laboratory experiments
Hoerz, F.↗
Runaway stars and the pulsars near the Crab Nebula
Runaway stars and pulsars near Crab Nebula, discussing binary system explosion and remnant motion
Gott, J. R., III↗
Statistical mechanics of supernovae
Galactic cosmic rays origin in terms of statistical mechanical model of supernova explosions
Jones, F. C.↗
Growth phase of magnetospheric substorms
Magnetospheric substorms model modification for growth phase inclusion prior to explosive expansion phase
Mcpherron, R. L.↗
Improved method of using paraformaldehyde as a disinfectant
Paraformaldehyde decreases required enclosed compartment disinfectant time and temperature by vaporizing powdered material from water slurry. Fire and explosion hazard at lower temperature is reduced. Total mixture evaporation occurs at plate temperature of approximately 167 deg K below that required to vaporize powdered material.
Milner, J. F.↗
Synthesis of fluorinated organic compounds using oxygen difluoride
Oxygen difluoride synthesis is a much simpler, higher-yield procedure than reactions originally followed to synthesize various fluorinated organic compounds. Extreme care is taken in working with oxygen difluoride as its reactions present severe explosion hazard.
Toy, M. S.↗
A study of high frequency nonlinear combustion instability in baffled annular liquid propellant rocket motors
Computer program contains mathematical model which provides relationship between engine gas dynamics and combustion processes. Mathematically simulated explosions initiate gas disturbances. Design methods for damping disturbances can be studied to prevent future engine shutdown or destruction.
Abreu, A.↗
On the dynamics of shock intersections
Dynamics of collisions between shock intersections and wave configurations in gases and condensed explosives
Kwak, D.↗
Feasibility of obtaining hypervelocity acceleration using propellant lined launch tubes Final report, 27 Sep. 1966 - 5 May 1970
Feasibility of explosive lining in launch tube for hypervelocity projectile acceleration
Rodenberger, C.↗
Aerospace systems pyrotechnic shock data - Ground test and flight. Volume 1 - Summary and analysis Final report, Jun. 1968 - Mar. 1970
Characteristics of shock loads on spacecraft structures produced by pyrotechnics and explosive devices - Vol. 1
Kacena, W. J., III↗
Aerospace systems pyrotechnic shock data /ground test and flight/. Volume 3 - Data Final report, Jun. 1968 - Mar. 1970
Determination of shock loads on spacecraft structures created by explosive separation of components - Vol. 3
Kacena, W. J., III↗
Aerospace systems pyrotechnic shock data /ground test and flight/. Volume 4 - Lockheed data and analyses Final report, Jun. 1968 - Mar. 1970
Compilation of shock loads on spacecraft structures produced by actuation of pyrotechnics and explosive devices - Vol. 4
Kacena, W. J., III↗
Aerospace systems pyrotechnic shock data /ground test and flight/. Volume 5 - Lockheed data and analyses Final report, Jun. 1968 - Mar. 1970
Characteristics of shock loads induced on spacecraft structures by initiation of explosive pin pullers - Vol. 5
Kacena, W. J., III↗
Aerospace systems pyrotechnic shock data /ground test and flight/. Volume 6 - Pyrotechnic shock design guidelines manual, revision A Final report, Jun. 1968 - Mar. 1970
Design of structures and equipment to reduce shock loads induced by pyrotechnics and explosive devices - Vol. 6
Kacena, W. J., III↗