The hybrid patched conic applied to lunar return trajectory propagation
Hybrid patched conic iterative technique for accurate moon-earth /transearth/ trajectory generation
Escobal, P. R.↗
Engineering topics
Stern, G. S.
Publications and source records attributed to Stern, G. S..
The hybrid patched conic technique as applied to the lunar trajectory problem
Hybrid patched conic technique as iterative procedure for generating translunar and transearth trajectories emphasizing computing time saving
Escobal, P. R.↗
Optimum deorbit positioning for minimum impulse reentry.
Optimum deorbit positioning on planetocentric elliptic orbit for single impulse reentry treated by two coupled quartic polynomials
REENTRY PHYSICS↗
Optimum deorbit positioning for minimum impulse reentry.
Optimum deorbit positioning on planetocentric elliptic orbit for single impulse reentry treated by two coupled quartic polynomials
ELLIPTICAL ORBIT↗