Simple method of using onboard optical measurements to predict the orbit established after the lunar-ascent-transfer orbit
Onboard optical measurements of angles for orbit prediction established after lunar-ascent and transfer orbits
Baker, L. K.↗
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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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Aerodynamic and rocket-exhaust heating during launch and ascent NASA space vehicle design criteria /Structures/
Aerodynamic and rocket exhaust heating during launch and ascent
Source record↗
The ascent environment
Aerodynamic heating, vibration, shock, and random noise environments during spacecraft ascent
Singletary, J. B.↗
Decompression procedures for the safe ascent of aerospace personnel from ground level to altitude, supplement A Final report
Decompression tables for safe ascent of aerospace personnel from level to level
Schreiner, H. R.↗
Decompression procedures for the safe ascent of aerospace personnel from ground level to altitude, supplement B Final report
Repetitive diving/flying decompression table for safe ascent to cabin pressure altitudes
Schreiner, H. R.↗
Apollo lunar descent and ascent trajectories
Apollo lunar descent and ascent trajectories
Bennett, F. V.↗
Revised Lunar Module Ascent Stage Thermal Model handbook
Revised Lunar Module Ascent Stage Thermal Model handbook
De Laughter, D. A.↗
Apollo 9 LM-3 ascent propulsion system, final flight evaluation
Steady state performance analysis for ascent propulsion system during Apollo 9 mission burn to depletion
Griffin, W. G.↗
RTCC requirements for Mission G - Selecting and verifying USBS Doppler data sources during LM ascent and descent
High speed Doppler tracking residuals for lunar module descent and ascent
Wylie, A. D.↗
Apollo 10 LM-4 ascent propulsion system, final flight evaluation
Lunar module ascent propulsion system performance for Apollo 10 mission
Griffin, W. G.↗
A study of lunar module navigation systems accuracies for powered decent, ascent, and aborts. Project Apollo
Lunar module navigation systems accuracies for powered descent, ascent, and abort trajectories
Henson, J. R.↗
Wind loads during ascent
Determining wind induced structural loads on space vehicle during ascent
Source record↗
Lunar descent and ascent trajectories
Apollo 11 premission planning, real time situation and postflight analysis for lunar descent and ascent phases, providing navigation correction capability for Apollo 12
Bennett, F. V.↗
A guidance system for the ascent of a Martian probe
Radio command guidance system for Mars probe ascent from surface to rendezvous with flyby vehicle on escape trajectory
Heffron, W. G., Jr.↗
Some new results on space shuttle atmospheric ascent optimization
Atmospheric ascent optimal trajectories for medium to high lift drag ratio space shuttle type rocket vehicles
Brown, K. R.↗
Buffeting during atmospheric ascent - Space vehicle design criteria /structures/
Aeroelastic spacecraft design to minimize buffeting during atmospheric ascent
Cole, H. A.↗
Thorad-Agena ascent and Agena orbital performance evaluation for Space Electric Rocket Test 2 /SERT 2/ mission
Evaluation of Thorad-Agena systems during ascent to orbit and Agena orbital performance during SERT 2 mission
Source record↗
Aerodynamic characteristics of a booster and an ascent shuttle configuration from Mach 0.28 to Mach 10.4
Wind tunnel tests to determine aerodynamic characteristics of booster and ascent shuttle configuration from Mach 0.28 to 10.4
Bernot, P. T.↗