Sa-8 operational trajectory
Trajectory optimization for Saturn I /SA-8/ LAUNCH vehicle to place S- IV stage and payload in elliptical orbit
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Trajectory optimization for Saturn I /SA-8/ LAUNCH vehicle to place S- IV stage and payload in elliptical orbit
Postflight trajectory analysis and orbital flight discussion for Saturn I /SA- 9/ launch vehicle carrying Pegasus payload
Trajectories for launch vehicles and approximate solution for propagation of covariance matrix of errors through thrust and coast
Sighting data and trajectory analysis for mission to periodic comets
Method for numerical solutions of nonlinear optimum trajectory problems using approximate analytic method
Approximation optimal trajectories - selection of estimation variables in least squares program, and computer program application
Trajectory and guidance analysis for flyby mission to comet and close-approach asteroid
Lunar Orbital Rendezvous - manned lunar landing trajectory and rendezvous
Statistical, trajectory, and sighting analysis for first-apparition comets - flight path parameters - astronomy
Approximation method using Euler-Lagrange equation for trajectory optimization
Motion constants for optimal thrust trajectories in central force field by iterative procedure
Double conic interplanetary trajectories to achieve optimum round trip with specified trip time and stay time for Mars mission
Earth Moon trajectories with consecutive collisions treated, using Birkhoff transformation in planar restricted three-body problem
Aerodynamic braking trajectories for Mars orbit attainment, giving entry corridors for lifting vehicles
Approximate analytical solutions of particle trajectories in model current sheets where electric field is uniform, perpendicular to magnetic field
Low thrust trajectory optimization, using Newton- Raphson method to solve nonlinear two-point boundary value problem
Low thrust satellite transfer between Earth and Moon orbits based on two-body trajectories and systematic synthesizing process
Trajectory characteristics resulting from stage- vehicle separation in near earth orbits