Add to ORKGThe prelaunch, lift-off, and midboost conditions that are important to the design of spacecraft are described. Original Apollo design concepts that were deficient in realistic and accurate analysis of spacecraft structural loads in a wind environment also are included. Important improvements in design criteria, mathematical models, wind-monitoring procedures, and loads analyses are discussed. Recommendations for future programs are presented
Analysis of loads produced on spacecraft by staging operations and practices to insure that staging ...
Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...
The conceptual aspects of the command and service module entry monitor subsystem, together with an i...
The flightworthiness of the Apollo spacecraft structure was verified primarily through a rigorous, v...
Analyses were performed to determine the structural loads caused by maneuvers of the docked Apollo c...
The problems encountered and the experience gained in the entry mission plans, flight software, traj...
The problem areas encountered during the development of the acceptance testing and preflight checkou...
The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superor...
A brief discussion of the development of the Apollo earth landing system and a functional descriptio...
This report describes the process of crew procedures development used in the Apollo Program. The two...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The development of flight-control facilities for the Apollo program is reviewed from the viewpoint o...
The development of the Apollo digital autopilots (the primary attitude control systems that were use...
A review of the Apollo spacecraft certification (qualification) test program is presented. The appro...
Analysis of loads produced on spacecraft by staging operations and practices to insure that staging ...
Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...
The conceptual aspects of the command and service module entry monitor subsystem, together with an i...
The flightworthiness of the Apollo spacecraft structure was verified primarily through a rigorous, v...
Analyses were performed to determine the structural loads caused by maneuvers of the docked Apollo c...
The problems encountered and the experience gained in the entry mission plans, flight software, traj...
The problem areas encountered during the development of the acceptance testing and preflight checkou...
The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superor...
A brief discussion of the development of the Apollo earth landing system and a functional descriptio...
This report describes the process of crew procedures development used in the Apollo Program. The two...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The development of flight-control facilities for the Apollo program is reviewed from the viewpoint o...
The development of the Apollo digital autopilots (the primary attitude control systems that were use...
A review of the Apollo spacecraft certification (qualification) test program is presented. The appro...
Analysis of loads produced on spacecraft by staging operations and practices to insure that staging ...
Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...
The conceptual aspects of the command and service module entry monitor subsystem, together with an i...