A DISCUSSION OF GUIDANCE POLICIES FOR MULTIPLE-IMPULSE CORRECTION OF THE TRAJECTORY OF A SPACECRAFT
Guidance policies for multiple-impulse correction of spacecraft trajectory
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Guidance policies for multiple-impulse correction of spacecraft trajectory
Two-impulse orbital transfer problem for elliptical orbits, describing techniques for finding optimum transfers and optimum rendezvous trajectories
Trajectory parameters for escaping from & braking into earth orbit utilizing single vehicle stage with high specific impulse
Impulse orbital transfer for nearly tangent coplanar elliptical orbits
Development of geomagnetic storms after negative sudden impulse
Tri-electrode cold cathode X-ray impulse tube of simple construction and low operating voltage
Numerical determination of optimum two-impulse orbital transfer between inclined elliptical orbits
Numerical and analytical results on optimum one impulse transfer between coplanar elliptical orbits
Effect of thrust-weight ratios and specific impulses on trajectory parameters for earth orbit hyperbolic escape and entry
Minimum propellant consumption trajectories to Mars for constant-thrust, constant-specific impulse vehicles with optimum coasting periods
Sublimating-solid micropropulsion impulse and thrust tests using integrating microthrust balance
Optimum transfer between two terminal points for minimum initial impulse under arbitrary initial velocity vector
Optimal free-space fixed thrust trajectories using impulsive trajectories as starting iteratives
Impulses originating in dendrite region in most dorsal part of dorsal horn, noting correlation between membrane potential and cell firing rate
Liquid cooled high specific impulse arc jet engine has measured engine thrust not completely aerodynamic in nature
Optimal free-space fixed thrust trajectories using impulsive trajectories as starting iteratives
Optimal multiple impulse orbital rendezvous
Analytic solution for minumum impulse transfer between two neighboring low eccentricity orbits