Add to ORKGEngineering specifications of a trace contaminant control system designed for the Space Station Prototype (SSP) were given. These were divided into two appendices: (1) a list of nonmetallic materials used, and (2) engineering drawings of the overall system, sub-assemblies, and components
The author had identified the following significant results. Repeated looks at surfaces that maintai...
Structural adhesives prepared from fluorinated polyurethanes for use with liquid oxyge
The design and development of a safety and arming device for the space shuttle solid rocket booster ...
Drawings are presented for equipment designed and fabricated to affect the integration of controller...
The final nonmetallic materials summary for the Apollo ultraviolet spectrometer experiment lists man...
In 1982 a workshop was held to refine the science rationale for large deployable reflectors (LDR) an...
The control parameters are defined which are to be used by the Photographic Technology Division for ...
Elastomeric products were developed for use in the space shuttle program, and investigations were co...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
The design and performance of pointing and control systems for two space infrared telescope facility...
A flight test program was conducted in which the effects of various surface coatings on aerodynamic ...
As the Space Station nears reality in funding support from Congress, NASA plans to perform over a hu...
A handbook compilation of chemical and physical property tests data obtained during qualification an...
A series of tests was performed to determine an optimum resin to be used as a UV rigidizable matrix ...
The author had identified the following significant results. Repeated looks at surfaces that maintai...
Structural adhesives prepared from fluorinated polyurethanes for use with liquid oxyge
The design and development of a safety and arming device for the space shuttle solid rocket booster ...
Drawings are presented for equipment designed and fabricated to affect the integration of controller...
The final nonmetallic materials summary for the Apollo ultraviolet spectrometer experiment lists man...
In 1982 a workshop was held to refine the science rationale for large deployable reflectors (LDR) an...
The control parameters are defined which are to be used by the Photographic Technology Division for ...
Elastomeric products were developed for use in the space shuttle program, and investigations were co...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
The design and performance of pointing and control systems for two space infrared telescope facility...
A flight test program was conducted in which the effects of various surface coatings on aerodynamic ...
As the Space Station nears reality in funding support from Congress, NASA plans to perform over a hu...
A handbook compilation of chemical and physical property tests data obtained during qualification an...
A series of tests was performed to determine an optimum resin to be used as a UV rigidizable matrix ...
The author had identified the following significant results. Repeated looks at surfaces that maintai...
Structural adhesives prepared from fluorinated polyurethanes for use with liquid oxyge
The design and development of a safety and arming device for the space shuttle solid rocket booster ...