Self-rescue during EVA is examined in terms of the use of a hand-held thruster that is similar to the hand-held maneuvering units HHMU developed for earlier programs. The problem of assessing velocity-increment requirements is addressed by means of examples of simulation technologies for studying EVA. The technologies evaluated include virtual reality systems such as the Virtual Interactive Environment Workstation (VIEW) and the Space Operations Simulator, and standard approaches like the air-bearing floor and the space shuttle. The VIEW is employed for a study of five trained NASA subjects that conduct a simulated return to a spacecraft with an HMMU under variable conditions. The study demonstrates the efficacy of VIEW for obtaining fuel-consumption values, and separation velocity is identified as the most significant determinant of the fuel and time requirements for a self-rescue operation.
Simulation of extra-vehicular activity (EVA) self-rescue
1991-07-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Simulation of Extra-Vehicular Activity (EVA) Self-Rescue
SAE Technical Papers | 1991
|Space Shuttle Extra Vehicular Activity
NTIS | 1994