국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Space Suit Portable Life Support System Test Bed (PLSS 1.0) Development and Testing
저자	Watts, Carly;; Campbell, Colin;; Vogel, Matthew;; Conger, Bruce
Keyword	EVAPORATORS;; FLEXIBILITY;; HEAT RADIATORS;; MEMBRANES;; MOBILITY;; OXYGEN REGULATORS;; PORTABLE LIFE SUPPORT SYSTEMS;; PROTOTYPES;; SPACE SUITS;; SYSTEMS ENGINEERING;; TEMPERATURE CONTROL;; TEST STANDS;; VENTILATION
URL	http://hdl.handle.net/2060/20120007410
보고서번호	JSC-CN-26247
발행년도	2012
출처	NTRS (NASA Technical Report Server)
ABSTRACT	A multi-year effort has been carried out at NASA-JSC to develop an advanced extra-vehicular activity Portable Life Support System (PLSS) design intended to further the current state of the art by increasing operational flexibility, reducing consumables, and increasing robustness. Previous efforts have focused on modeling and analyzing the advanced PLSS architecture, as well as developing key enabling technologies. Like the current International Space Station Extra-vehicular Mobility Unit PLSS, the advanced PLSS comprises three subsystems required to sustain the crew during extra-vehicular activity including the Thermal, Ventilation, and Oxygen Subsystems. This multi-year effort has culminated in the construction and operation of PLSS 1.0, a test bed that simulates full functionality of the advanced PLSS design. PLSS 1.0 integrates commercial off the shelf hardware with prototype technology development components, including the primary and secondary oxygen regulators, Ventilation Subsystem fan, Rapid Cycle Amine swingbed carbon dioxide and water vapor removal device, and Spacesuit Water Membrane Evaporator heat rejection device. The overall PLSS 1.0 test objective was to demonstrate the capability of the Advanced PLSS to provide key life support functions including suit pressure regulation, carbon dioxide and water vapor removal, thermal control and contingency purge operations. Supplying oxygen was not one of the specific life support functions because the PLSS 1.0 test was not oxygen rated. Nitrogen was used for the working gas. Additional test objectives were to confirm PLSS technology development components performance within an integrated test bed, identify unexpected system level interactions, and map the PLSS 1.0 performance with respect to key variables such as crewmember metabolic rate and suit pressure. Successful PLSS 1.0 testing completed 168 test points over 44 days of testing and produced a large database of test results that characterize system level and component performance. With the exception of several minor anomalies, the PLSS 1.0 test rig performed as expected;; furthermore, many system responses trended in accordance with pre-test predictions.