Add to ORKGThe problems encountered and the experience gained in the entry mission plans, flight software, trajectory-monitoring procedures, and backup trajectory-control techniques of the Apollo Program should provide a foundation upon which future spacecraft programs can be developed. Descriptions of these entry activities are presented. Also, to provide additional background information needed for discussion of the Apollo entry experience, descriptions of the entry targeting for the Apollo 11 mission and the postflight analysis of the Apollo 10 mission are presented
The Apollo launch escape propulsion subsystem contained three solid rocket motors. The general desig...
Definition of a practical return-to-earth abort capability was required for each phase of an Apollo ...
The Apollo spacecraft Problem Reporting and Corrective Action System is presented. The evolution fro...
The problems encountered and the experience gained in the entry mission plans, flight software, traj...
This report describes the process of crew procedures development used in the Apollo Program. The two...
The conceptual aspects of the command and service module entry monitor subsystem, together with an i...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The history of flight planning for manned space missions is outlined, and descriptions and examples ...
The premission planning, the real-time situation, and the postflight analysis for the Apollo 11 luna...
The development of a computerized capability to depict views from the Apollo spacecraft during a lun...
The problem areas encountered during the development of the acceptance testing and preflight checkou...
The evolution of the nominal rendezvous-maneuver plan for the lunar landing missions is presented al...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
The development of the guidance targeting techniques for the Apollo command module and launch vehicl...
An unmanned test flight program required to evaluate the command module heat shield and the structur...
The Apollo launch escape propulsion subsystem contained three solid rocket motors. The general desig...
Definition of a practical return-to-earth abort capability was required for each phase of an Apollo ...
The Apollo spacecraft Problem Reporting and Corrective Action System is presented. The evolution fro...
The problems encountered and the experience gained in the entry mission plans, flight software, traj...
This report describes the process of crew procedures development used in the Apollo Program. The two...
The conceptual aspects of the command and service module entry monitor subsystem, together with an i...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The history of flight planning for manned space missions is outlined, and descriptions and examples ...
The premission planning, the real-time situation, and the postflight analysis for the Apollo 11 luna...
The development of a computerized capability to depict views from the Apollo spacecraft during a lun...
The problem areas encountered during the development of the acceptance testing and preflight checkou...
The evolution of the nominal rendezvous-maneuver plan for the lunar landing missions is presented al...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
The development of the guidance targeting techniques for the Apollo command module and launch vehicl...
An unmanned test flight program required to evaluate the command module heat shield and the structur...
The Apollo launch escape propulsion subsystem contained three solid rocket motors. The general desig...
Definition of a practical return-to-earth abort capability was required for each phase of an Apollo ...
The Apollo spacecraft Problem Reporting and Corrective Action System is presented. The evolution fro...