The effect of thermal escape on the neutral hydrogen density above 120 kilometers.
Effect of thermal escape on neutral hydrogen density above 120 km
JEANS THEORY↗
SEARCH · Engineering Papers
Results for “ESCAPE”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Escape corrections for X-ray spectra of celestial sources.
Crab Nebula X-ray spectrum from balloon observations, noting importance of correction for escaped iodine K component
CELESTIAL OBSERVATION↗
Simulated gravity - the aversive stimulus in an escape and punishment situation.
Criterion of aversiveness to test effectiveness of simulated gravity as aversive stimulus in escape and punishment situation with squirrel monkeys, samiri sciurea
GRAVITY↗
Correction of balloon X-ray astronomy data for the effects of atmospheric attenuation, K X-ray escape, and energy resolution
Correction of balloon X ray astronomy data for atmospheric attenuation, escape, and energy resolution
Overbeck, J. W.↗
Transonic aerodynamic characteristics of powered models of several Apollo launch- escape vehicle configurations
Effects of simulated jet exhaust flow on transonic aerodynamic characteristics of Apollo launch escape vehicle models
Berrier, B. L.↗
Development of the Apollo launch escape system.
Apollo launch escape system, discussing digital computer programs and wind tunnel program
Crowder, R. S.↗
Optimum three-impulse transfer between an elliptic orbit and a non-coplanar escape asymptote.
Optimum three impulse transfer mode of escape from elliptic orbit to noncoplanar hyperbolic asymptote
Gerbracht, R. J.↗
Nonlocal energy deposition in the ionosphere and the photoelectron escape flux.
Nonlocal energy deposition in ionosphere without thermal equilibrium among neutral, ion and electron gases and photoelectron escape flux
Whitten, R. C.↗
Photoelectron escape from the ionosphere.
Photoelectron escape from ionosphere to magnetosphere, noting flux dependence on energy and factors affecting transport equations and protonosphere heating
Nisbet, J. S.↗
Two-burn escape maneuvers with an intermediate coasting ellipse
Two burn spacecraft trajectories for escaping earth parking orbit
Willis, E. A., Jr.↗
Aerodynamic loads on deployed canard surfaces and rocket nose section of the Apollo launch escape vehicle
Aerodynamic loads on deployed canard surfaces and rocket nose section of Apollo launch escape vehicle
Moseley, W. C., Jr.↗
Aerodynamic characteristics determined during development of the Apollo launch escape vehicle configuration
Aerodynamic characteristics determined during development of Apollo launch escape vehicle configuration in wind tunnel tests
Bowen, F. E.↗
Escape of atmospheric helium by nonthermal processes.
Atmospheric helium nonthermal escape mechanisms, noting ion loss from polar ionosphere
Patterson, T. N. L.↗
Avoidance and escape behavior controlled by artificial gravity.
Squirrel monkeys escape behavior under centrifuge simulated gravity in excess of earth gravity
Belleville, R. E.↗
The escape of light from within a massive star
Escape of light from within spherically symmetric gravitational masses
Jaffe, J.↗
Wind-tunnel investigation of the aerodynamic pressures on the Apollo launch escape vehicle configuration
Wind tunnel investigation of aerodynamic pressures on Apollo launch escape vehicle configuration
Moseley, W. C., Jr.↗
Lunar Escape Systems /LESS/ feasibility study. Volume 1 - Summary report
Feasibility study of lunar emergency escape-to-orbit system
Matzenauer, J. O.↗
The effects of wind forces on a thrusting launch vehicle and launch escape system for Apollo mode 1 aborts
Effects of wind forces on thrusting launch vehicle and launch escape system for Apollo mode 1 aborts
Dietrick, D. L.↗