OGO 3 observations of the Lyman alpha intensity and the hydrogen concentration beyond 5 R sub E
Lyman alpha intensity and hydrogen concentration at 5 to 19 earth radii determined from OGO 3 spacecraft measurements
Mange, P.↗
SEARCH · Engineering Papers
Results for “E”
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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Liquid rocket technology for the ch. e.
Liquid rocket technology for chemical engineers, discussing propellant tanks, lines and valves, tank pressurization, turbopumps and combustion chamber problems
Priem, R. J.↗
On the dependence of T sub e upon quantity versus quality of the radiation field in a stellar atmosphere
Stellar atmosphere radiation field quantity vs quality, deriving electron temperature as function of tau
Gebbie, K. B.↗
Investigation of the D and E regions of the ionosphere quarterly progress report, 1 Oct. 1968 - 30 Sep. 1969
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Source record↗
Investigations of the D and E regions of the ionosphere Monthly progress reports 1-4, 1 Oct. 1969 - 31 Jan. 1970
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Smith, L. G.↗
Antenna and propagation studies for spacecraft task E-53F - An analysis of the ranging system for the lunar surface electral properties experiment
Analysis of ranging system for lunar surface electrical properties experiment
Osborn, J. D.↗
Plasma Probe C, D, and E, volume 1 Final engineering report
Plasma probe for Pioneer spacecraft to measure ion and electron density and angular distribution in space
Aalami, D.↗
Plasma Probe C, D and E, volume 2 Final engineering report
Integrated circuits for digital applications in high dc noise systems
Source record↗
Relation of the plasmapause position to the region of enhanced fluxes of trapped energetic (E greater than 280 keV) electrons during the 15 June 1965 magnetic storm
Relation of plasmapause position to region of enhanced fluxes of trapped energetic electrons during magnetic storm on 15 June 1965
Arens, J. F.↗
Performance verification of the lunar descent program - P66 auto, task E-72C
Results of simulated runs to evaluate lunar module descent performance of P66 automatic control and guidance system
Dwivedi, N. P.↗
Energetic particle flux experiment /AIMP-D and E/ Final report, 28 Jan. - 31 Oct. 1969
Analyzing data from Explorer 33 and 35 on energetic solar particles in interplanetary medium and terrestrial particle fluxes in magnetopause bow shock regions
Source record↗
Apollo RCS positive expulsion tankage product improvement program - Solution of command module and service module bladder repositioning problems, task E Final report, Jul. 1967 - Sep. 1969
Solution of command module and service module expulsion bladder repositioning problems
Source record↗
Sizing data for multiple stages. Expended and reusable operating modes. Tabular listing of configuration Delta V capabilities, appendix A Project technical report, task E-94
One way velocity increments obtainable from one and two stage propulsive configurations for expended and reusable modes - tables
Bratkowski, R. J.↗
Stage sizing data for an unmanned planetary sample return mission, task E-94 Project technical report
Outbound and inbound stage weight requirements for planetary sample return mission payload and energy requirements - graphs
Gilbertson, R. D.↗
Comparison of lunar gravity fields using GSFC range-rate data from AIMP-E
Application of VHF Doppler tracking data from Goddard Range and Range Rate system to determine lunar orbits for Explorer 35 satellite
Laczo, V. T.↗
Development of CO2 laser Doppler instrumentation detection of clear air turbulence Appendix D and appendix E, addenda to final report
Clear air turbulence pulse Doppler laser radar design including analysis of mechanical vibration effects on laser transmitter and reciever
Jelalian, A.↗
From Apollo 11 to the Space Stations of the Future: Space and Aviation: Lecture No. 12 - Session E
Predictions and recommendations for development and deployment of manned space stations
Cohen, H.↗