Summary of spacecraft range safety trajectory analyses for Apollo missions - Project Apollo
Summary of spacecraft range safety trajectory analyses for Apollo missions
Kincade, R. E.↗
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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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An envelope of Saturn 5 malfunction trajectories which can achieve orbit - Project Apollo
Malfunctions defining impending abort situation for Saturn 5 launch trajectory to attain contingency orbit
Dulock, V. A.↗
Excessive entry loads for abort trajectories for the nominal AS-205/101 launch profile
Excessive entry loads for abort trajectories from nominal AS-205/101 launch profile
Henderson, E. M.↗
Space shuttle trajectory management, navigation, guidance, and control during approach and landing Interim report
Trajectory control and optimization for space shuttle approach and landing
Source record↗
Optimal trajectory management for the space shuttle
Post-reentry trajectory optimization for space shuttles
Desai, M.↗
Applications of optimization theory to space shuttle trajectory control in the subsonic regime
Energy and accuracy factors in feedback path control system design for optimizing space shuttle trajectory control at subsonic speed
Mac Kinnon, D.↗
Launch phase abort analysis for a 50 deg orbital inclination trajectory
Launch phase abort analysis for ascent to orbit trajectory
Source record↗
Aircraft simulation of lunar landing approach trajectories
Aircraft simulation of lunar excursion module landing approach trajectories
Stegall, J. F.↗
A two-dimensional digital computer program for calculation of optimum trajectories from launch to injection
Equations of motion for two dimensional digital computer program for calculation of optimum trajectories from launch to injection
Bone, E. D.↗
Application of the matched conic model in the study of circumlunar trajectories. Project Apollo
Matched conic model and integrated circumlunar trajectories compared at injection, pericynthion and perigee
Gibson, T. F., Jr.↗
Analytic formulation of three wedge angle constraints in trajectory studies
Analytic formulation of three wedge angle constraints in trajectory studies
Laszlo, W. O.↗
Guidance laws for controlling off-nominal LM powered descent trajectories back to the nominal. Project Apollo
Guidance laws for controlling LM powered descent trajectories
Mc Swain, G. G.↗
Parametric design of interplanetary and orbital trajectories with examples for Mars 1973, 1975, and 1977 opportunities
Parametric design of interplanetary and orbital trajectories with examples for Mars 1973, 1975, and 1977 opportunities
Hampshire, W. F., II↗
Solar electric interplanetary trajectory and performance data for sub-optimal powered spacecraft
Trajectory and spacecraft design data for unmanned interplanetary missions using suboptimal powered solar electric propulsion
Horsewood, J. L.↗
Trajectory Application Method /TAM/
Trajectory Application Method simulation program for postflight propulsion system performance evaluation on Saturn S-1B stage
Sheats, J. P.↗
A method for computing extremal maximum-range thrust-limited rocket trajectories with application to lunar transport
Extremal, maximum-range, thrust limited rocket trajectory computing method with lunar transport applications
Armstrong, E. S.↗
Optimum trajectories to circular synchronous equatorial orbit for smaller-than-optimum apogee motors
Optimum trajectories to circular synchronous equatorial orbit for smaller than optimum apogee motors
Spurlock, O. F.↗
Optimal three dimensional reentry trajectories for Apollo-type vehicles
Numerical optimization method based on perturbation theory for calculating optimal three dimensional reentry trajectories for Apollo type vehicles
Williamson, W. E., Jr.↗