Development of space station window assemblies
Explosively cut space station window assemblies prototype development
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Explosively cut space station window assemblies prototype development
The development of very large size solid rocket engines cannot be accomplished, as in the case of small rocket engines, by empirical methods requiring a great number of full-scale firings. It is therefore necessary to predict rocket operation from data obtained on charges of different size and geometry. This paper presents a mathematical method for determining analytically the rocket engine thrust and chamber pressure development curves from the charge and engine geometry, the heat of explosion the kinetics characteristics and any other parameters affecting engine operation. It is shown that it is possible to compute empirical values for burning rate and erosion effects from experimental firings. Following a brief survey of the fundamentals of this method, the procedure is illustrated by four representative examples.
Detonation wave initiation in gaseous media, noting transition process for flames accelerating to detonation and explosions behind reflected shock wave
Saturn fireball thermal environment associated with liquid propellant explosions, using analytical model
Mixing function vs time relationship for liquid propellant explosion hazards prediction, noting thermocouple grid for maximum information
Acoustic and electromagnetic energy propagation in lower ionosphere and atmosphere for energy pulse generation by chemical explosion
Gamma ray telescope development for balloon-borne astronomy in search for discrete gamma sources and supernova explosions
Magnetospheric substorm as discharge process of associated electric current system, discussing relaxation processes, explosive release of energy, etc
Oxide composition of silicate spherules from forest area devastated by Tunguska meteorite explosion using electron microprobe analysis
Shock tube with cylindrical explosive to implode glass wall and produce high velocity glass particle jet, studying jet velocity and behavior and test gas pressure effects
Gage permits determination of stagnation conductivity from measurement of shunt impedance presented by the plasma between the inner and outer conductors of a segment of coaxial transmission line. Response of gage permits its use in shock-tube work and research on explosive propagation.
Analytical technique is developed for prediction of reverse buckling in thin curved shells. Test data indicate technique predicts actual reverse buckling pressure within 10 percent, and should be useful for analytical prediction of reversed condition failure for problems such as explosive decomposition through vacuum failure.
Hypervelocity meteorite impacts by nuclear and chemical explosions
Theoretical and applied seismology, earthquake engineering, earth structure, industrial uses, facilities, and underground nuclear explosion detection
Detonation wave striking PETN explosive shell producing implosion or implosion wave in shock tube
High energy electromagnetic radiation and energetic particles from sun, galaxies, and nuclear explosions in spacecraft environment
Space radiation effects on organic fluids, photographic emulsion, propellants, and explosives
Electric discharge apparatus for electrohydraulic explosive forming