1983-07-11

Regenerable Non-Venting Thermal Control Subsystem for Extravehicular Activity, 1983 831151

With the advent of manned spacecraft opportunities requiring routine and complex extravehicular activities (EVA) a new concept for heat rejection is mandatory in order to realize maximum crewmember productivity. An optimum extravehicular mobility unit (EMU) thermal control system must be capable of successful operation without requiring expendables and without introducing contaminants into the environment, and be readily regenerable.
This paper presents a regenerable non-venting thermal control subsystem requirements specification generated for a Shuttle-related EMU, identifies candidate concepts capable of fulfilling the requirements for each thermal control subsystem application, evaluates each candidate concept with respect to the subsystem requirements, and selects the best approach for each requirement.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Digital Optical Based Aircraft Actuator Controller Utilizing SiC Power Switches

2012-01-2238

View Details

JOURNAL ARTICLE

Advanced Electric Drives for Aerospace More Electric Architectures

2008-01-2861

View Details

TECHNICAL PAPER

EVA Space Suit Glove: Experiences and Main Design Problems

981632

View Details

X