Ballistic range tests of ablating and nonablating slender cones.
Ballistic range tests to study ablation effects on aerodynamic characteristics of ablating and nonablating slender cones
Chapman, G. T.↗
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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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Development of the ballistic rocket concept for rocket climatology
Ballistically effective atmospheric parameters for rocket vehicle design manuals involving application of climatological concepts of meteorology
Reisig, G. H. R.↗
Ballistic wake of turbulence in a plasma shock wave.
Ballistic wake structure and jump conditions for plane plasma shock waves with electrostatic turbulence
Krall, N. A.↗
Simplified ballistic-limit expressions for thin sheets
Ballistic limit thickness of thin plate
Weidman, D. J.↗
Capability of NOL ballistics ranges for obtaining sphere drag coefficient data
Ballistic ranges for measuring drag coefficients of spheres
Lyons, W. C., Jr.↗
Development and testing of a ballistic impact loading device
Development and testing of ballistic shock loading device with projectile for producing stress waves in polymethyl methacrylate rods
Simonson, D. L.↗
Sequential estimation of states of a ballistic vehicle in an imperfectly known atmosphere
Least squares method for sequential guidance estimates on ballistic vehicle in partially known atmosphere
Bejczy, A. K.↗
Gas opacity measurements with a ballistic piston compressor
Ballistic piston compressor for opacity measurements of hot compressible gases
Hammond, G. L.↗
Determination of mean orbital elements from initial conditions for a Vinti ballistic trajectory
Mean orbital elements for Vinti spheroidal theory of drag-free satellite motion applied to ballistic trajectories
Walden, H.↗
A small ballistic range for impact metamorphism studies
Experimental ballistic range for shock loading of rock materials
Hoerz, F.↗
Interior ballistics of high-low propulsion systems
Interior ballistics of high-low propulsion system with fixed volume high pressure combustion chamber coupled to variable volume lower pressure action chamber
Heiney, O. K.↗
A terminal ballistics application of transmission electron microscopy - The anatomy of a bullet hole
Thin sheet and laminate bullet hole deformation zone microstructure observation by electron microscopy, considering terminal ballistics approach
Foltz, J. V.↗
Ballistic range tests of ablating and nonablating slender cones
Ballistic range tests to study ablation effects on aerodynamic characteristics of ablating and nonablating slender cones
Chapman, G. T.↗
Apollo 12 lunar module impact - Laboratory simulation and possible downrange ballistic effects
Apollo 12 lunar module impact laboratory simulation, investigating possible downrange ballistic effects and cratering process
Johnson, S. W.↗
Determination of mean orbital elements from initial conditions for a Vinti ballistic trajectory
Mean orbital element determination using Vintis spheroidal theory of drag-free satellite motion applied to ballistic trajectories
Walden, H.↗
Techniques for Optical Radiation Studies in the Ballistic Range
Techniques and instrumentation for optical radiation measurements in ballistic ranges
Page, W. A.↗
Effects of low-temperature ammonium perchlorate decomposition on the ballistic and physical properties of a CTPB propellant
Low temperature condensed phase ammonium perchlorate decomposition effects on ballistic and postheat sterilization properties of CTPB propellant
Cofer, W. R., III↗
The NOL ballistic piston compressor 2: Operation up to 5,000 ATM
Experiments are described which demonstrated the feasibility of rapidly compressing inert gases in a ballistic piston compressor to simultaneously high temperatures and densities previously unobtainable in the laboratory. With argon, temperatures of the order of 6000 K and accompanying densities of the order of 100 Amagats have been obtained; and with nitrogen, temperatures and densities of 3000 K and 400 Amagats have been approached. Details of the design, assembly, instrumentation, and operating procedures are presented, and the results of mechanical and thermal performance tests up to 5000 atmospheres pressure are described. Emphasis is placed on experiments which demonstrated the usefulness of this apparatus for spectral line broadening studies.
Hammond, G. L.↗