Add to ORKGThe feasibility of utilizing electrostatic forces for personnel retention devices on exterior spacecraft surfaces was analyzed. The investigation covered: (1) determination of the state of the art; (2) analysis of potential adhesion surfaces; (3) safety considerations for personnel; (4) electromagnetic force field determination and its effect on spacecraft instrumentation; and (5) proposed advances to current technology based on documentation review, analyses, and experimental test data
The requirements for mobility aids and restraint devices for use by personnel of the space shuttle w...
The interaction of the aerospace environment with spacecraft surfaces and onboard, high voltage spac...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
The experience is described of NASA and DOD with electrostatic problems, generation mechanisms, and ...
This program objectives were to produce a pressure measurements system that penetrates the thermal p...
Design and development of gravity substitute workbench using electrostatic and aerodynamic principle
The need for uniform criteria, or guidelines, to be used in all phases of spacecraft design is discu...
Experimental tube design, vacuum system, technique for studying electron and ion emission from cesia...
Magnetic torque resulting from interaction between magnetic properties of spacecraft and ambient mag...
Alternating current circuit breaker and direct current engine contactors for space - vacuum interru...
Tests were conducted to determine the effects of electrostatic propulsion beam divergence effects on...
Flight test and evaluative data relating to design and use of elastomeric shield materials for therm...
Alternating current circuit breakers and direct current engine contactors for space nuclear electric...
A compendium of techniques and basic information useful to the preliminary performance analysis of p...
Needs and requirements for a free flying space science and applications platform to host groupings o...
The requirements for mobility aids and restraint devices for use by personnel of the space shuttle w...
The interaction of the aerospace environment with spacecraft surfaces and onboard, high voltage spac...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
The experience is described of NASA and DOD with electrostatic problems, generation mechanisms, and ...
This program objectives were to produce a pressure measurements system that penetrates the thermal p...
Design and development of gravity substitute workbench using electrostatic and aerodynamic principle
The need for uniform criteria, or guidelines, to be used in all phases of spacecraft design is discu...
Experimental tube design, vacuum system, technique for studying electron and ion emission from cesia...
Magnetic torque resulting from interaction between magnetic properties of spacecraft and ambient mag...
Alternating current circuit breaker and direct current engine contactors for space - vacuum interru...
Tests were conducted to determine the effects of electrostatic propulsion beam divergence effects on...
Flight test and evaluative data relating to design and use of elastomeric shield materials for therm...
Alternating current circuit breakers and direct current engine contactors for space nuclear electric...
A compendium of techniques and basic information useful to the preliminary performance analysis of p...
Needs and requirements for a free flying space science and applications platform to host groupings o...
The requirements for mobility aids and restraint devices for use by personnel of the space shuttle w...
The interaction of the aerospace environment with spacecraft surfaces and onboard, high voltage spac...
Examination of commercial equipment technologies revealed that the functional performance requiremen...