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.↗
Engineering topics
Teren, F.
Publications and source records attributed to Teren, F..
Analysis of broken plane trajectories for the Pioneer-F mission
Pioneer-F Jupiter flyby mission planning, considering use of optimum broken plane trajectories to increase launch opportunity and/or payload capability
Teren, F.↗
Optimum launch trajectories for the ATS-E mission
Optimum launch trajectories for ATS-E mission with noncircular parking orbits, considering apogee motor size, perigee radius and duration constraints
Spurlock, O. F.↗
Analysis of broken plane trajectories for the Pioneer-F mission
Analysis of broken plane trajectories for Pioneer F mission
Teren, F.↗
Optimum launch trajectories for the ATS-E mission
Optimum launch trajectories for ATS-E mission
Spurlock, O. F.↗
Optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints
Mathematical models for optimal three dimensional launch vehicle trajectories with attitude and attitude rate constraints
Spurlock, O. F.↗
A wind profile for generating control requirements for rocket vehicles using liquid-injection control systems
Wind profile developed for calculation of deflection impulse for rocket with liquid injection thrust vector control
Daniele, C. J.↗
Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirements
Load relief autopilot to minimize launch vehicle thrust vector deflection angle required for vehicle stability during flight through design winds
Scalzott, L. L.↗
A trajectory code for maximizing the payload of multistage launch vehicles
Computer program for trajectory optimization and payload maximization in multistage launch vehicles
Spurlock, O. F.↗
Thrust-vector control requirements for large launch vehicles with solid-propellant first stages
Thrust vector control for large launch vehicles with solid propellant first stages
Borsody, J.↗
Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight
Thrust vector deflection stability analysis for minimum control requirements of booster vehicles during atmospheric flight
Borsody, J.↗
Analytical calculation of partial derivatives relating lunar and planetary midcourse correction requirements to guidance system injection errors
Two body equations of motion for calculating partial derivatives relating lunar and planetary midcourse correction requirements to guidance system injection errors
Cole, G. L.↗
Thrust vector control requirements for solid- propellant launch vehicles
Thrust vector deflection angle requirements for controlling solid propellant launch vehicle
THRUST VECTOR CONTROL /TVC/↗
Payload optimization of multistage launch vehicles
Payload optimization of multistage launch vehicle- generalized Bolza problem for maximal payload capability analysis
MULTISTAGE ROCKET VEHICLE↗
Explicit guidance equations for multistage boost trajectories
Explicit equations for steering Atlas-Centaur multistage launch vehicle to lunar trajectory
MULTISTAGE VEHICLE↗
A variational method for multistage launch vehicle optimization.
Calculus of variations method used to maximize payload capability for multistage launch vehicles
PAYLOAD MASS RATIO↗
A variational method for multistage launch vehicle optimization
Variational calculus methods used to maximize payload capability for multistage launch vehicles
LAUNCH VEHICLE↗