Add to ORKGAn investigation of a two-impulse plan for performing rendezvous on a once-a-day basis with a near-earth satellite station indicates that launch into rendezvous from slightly less than maximum satellite latitude is an unusually favorable circumstance in that no appreciable expense in mass ratio is incurred. In addition, it was found for the two-impulse maneuver employed in this study that the optimum angular travel of the ferry vehicle to rendezvous was considerably less than the 1800 transfer which is optimum for the two-impulse in-plane launch
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
Keeping a cluster of satellites within bounded relative distances requires active control, because n...
The compability of the nominal rendezvous sequence with low target orbits is addressed. It was found...
A study is made of the families of non-thrusting ascent trajectories during rendezvous with an orbit...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
Program determines if rendezvous in near space is possible, and performs an analysis to determine th...
A digital-computer simulation was made of the midcourse or ascent phase of a rendezvous between a fe...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.MIC...
Flight scheduling in planar two burn minimum fuel rendezvous of interceptor with target vehicle
Abstract: The problem of a rendezvous of two spacecrafts on the close near-circular orbits...
Simplified and accurate relative equations of motion for two impulse orbital rendezvou
This paper deals with the inception and evolution of the simultaneous launch countdown technique. Fu...
Effect of using two separate engines in lunar lander for direct-return rendezvous with vehicl
The current planning process for space shuttle rendezvous with a second Earth-orbiting vehicle is ti...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
Keeping a cluster of satellites within bounded relative distances requires active control, because n...
The compability of the nominal rendezvous sequence with low target orbits is addressed. It was found...
A study is made of the families of non-thrusting ascent trajectories during rendezvous with an orbit...
The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. Th...
Program determines if rendezvous in near space is possible, and performs an analysis to determine th...
A digital-computer simulation was made of the midcourse or ascent phase of a rendezvous between a fe...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.MIC...
Flight scheduling in planar two burn minimum fuel rendezvous of interceptor with target vehicle
Abstract: The problem of a rendezvous of two spacecrafts on the close near-circular orbits...
Simplified and accurate relative equations of motion for two impulse orbital rendezvou
This paper deals with the inception and evolution of the simultaneous launch countdown technique. Fu...
Effect of using two separate engines in lunar lander for direct-return rendezvous with vehicl
The current planning process for space shuttle rendezvous with a second Earth-orbiting vehicle is ti...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
The three-dimensional rendezvous between two spacecraft is considered: a target spacecraft on a circ...
Keeping a cluster of satellites within bounded relative distances requires active control, because n...
The compability of the nominal rendezvous sequence with low target orbits is addressed. It was found...