Add to ORKGA description of the construction and use of crew provisions and equipment subsystem items for the Apollo Program is presented. The subsystem is composed principally of survival equipment, bioinstrumentation devices, medical components and accessories, water- and waste-management equipment, personal-hygiene articles, docking aids, flight garments (excluding the pressure garment assembly), and various other crew-related accessories. Particular attention is given to items and assemblies that presented design, development, or performance problems: the crew optical alinement sight system, the metering water dispenser, and the waste-management system. Changes made in design and materials to improve the fire safety of the hardware are discussed
Through space-flight experience and the development of simulators to meet the associated training re...
The reliability of the Apollo spacecraft resulted from the application of proven reliability and qua...
Definition of a practical return-to-earth abort capability was required for each phase of an Apollo ...
A description of the construction and use of crew provisions and equipment subsystem items for the A...
The Apollo command module crew-couch/restraint and load-attenuation system was required to support a...
Crew equipment stowage and stowage arrangement in spacecraft are discussed. Configuration control in...
An overview of the evolution of the design and development of the Apollo command module and lunar mo...
The development and performance history of the Apollo extravehicular mobility unit and its major sub...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
This report describes the process of crew procedures development used in the Apollo Program. The two...
A review of the Apollo command and service module instrumentation subsystem is presented. The measur...
The evolution of crew-operated photographic equipment and the procedures for manned space-flight pho...
A review of the command and service module controls and displays subsystem is presented. The subsyst...
Pyrotechnic devices were used successfully in many systems of the Apollo spacecraft. The physical an...
An unmanned test flight program required to evaluate the command module heat shield and the structur...
Through space-flight experience and the development of simulators to meet the associated training re...
The reliability of the Apollo spacecraft resulted from the application of proven reliability and qua...
Definition of a practical return-to-earth abort capability was required for each phase of an Apollo ...
A description of the construction and use of crew provisions and equipment subsystem items for the A...
The Apollo command module crew-couch/restraint and load-attenuation system was required to support a...
Crew equipment stowage and stowage arrangement in spacecraft are discussed. Configuration control in...
An overview of the evolution of the design and development of the Apollo command module and lunar mo...
The development and performance history of the Apollo extravehicular mobility unit and its major sub...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
This report describes the process of crew procedures development used in the Apollo Program. The two...
A review of the Apollo command and service module instrumentation subsystem is presented. The measur...
The evolution of crew-operated photographic equipment and the procedures for manned space-flight pho...
A review of the command and service module controls and displays subsystem is presented. The subsyst...
Pyrotechnic devices were used successfully in many systems of the Apollo spacecraft. The physical an...
An unmanned test flight program required to evaluate the command module heat shield and the structur...
Through space-flight experience and the development of simulators to meet the associated training re...
The reliability of the Apollo spacecraft resulted from the application of proven reliability and qua...
Definition of a practical return-to-earth abort capability was required for each phase of an Apollo ...