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.↗
SEARCH · Search NASA
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 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.↗
Lunar escape systems /LESS/ feasibility study, volume 2 Final technical report
Lunar escape systems feasibility study
Matzenauer, J. O.↗
Concerning the influence of elastic scattering upon photoelectron transport and escape
Elastic scattering effect on photoelectron transport and escape in upper sunlit atmosphere
Banks, P. M.↗
Departures from Jeans' escape for H and He in the earth's atmosphere
Jeans escape rate error for atmospheric H and He attributed to perturbed velocity distribution function, using realistic atom-atom elastic scattering cross sections
Brinkmann, R. T.↗
Photoelectron escape flux observations at midlatitudes
Photoelectron production and escape flux at midlatitudes, using spectrometric measurements from ISIS-1 satellite
Heikkila, W. J.↗
Optimal low thrust escape viewed as a resonance phenomenon
Second order perturbation solution to modified optimal low thrust escape problem
Jacobson, R. A.↗
Emergency escape system Patent
Design and specifications of emergency escape system for spacecraft structures
Kinzler, J. A.↗
Effects of high fat diets on caloric intake, body weight, and heat escape responses in normal and hyperphagic rats
High fat diet effects on caloric intake, body weight, and heat escape responses in normal and hyperphagic rats
Lipton, J. M.↗
Qualification evaluation of the tower jettison motor for the Apollo spacecraft program launch escape system
Qualification tests of tower jettison motors for Apollo spacecraft program launch escape systems
Lee, B. J.↗
Fixed-base simulator investigation of lightweight vehicles for lunar escape to orbit with kinesthetic attitude control and simplified manual guidance
Piloted simulator investigation of lightweight vehicles for emergency lunar escape to orbit with kinesthetic attitude control and simplified manual guidance
Hurt, G. J., Jr.↗
Orbital escape device Patent
Development and characteristics of inflatable structure to provide escape from orbit for spacecrews under emergency conditions
Johnson, C. C.↗