1988-07-01

Material Compatibility Problems for Ammonia Systems 881087

Thermal management systems are currently being developed for application on large orbiting platforms, specifically the Space Station. Based upon its thermodynamic properties, ammonia was selected as a working fluid suitable to handle the power and heat rejection requirements of these systems. The Space Station's 30-year design life, minimum maintenance requirement, maximum reliability, and ammonia working fluid have led to new material compatibility issues. Although ammonia is a well understood fluid for ground-based refrigeration uses, it produced some unexpected results when applied to space-based heat transport systems.

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

Power Thermal Management System Design for Enhanced Performance in an Aircraft Vehicle

2010-01-1805

View Details

TECHNICAL PAPER

Impact of Heat Exchanger Location on Engine Performance

2012-01-2168

View Details

TECHNICAL PAPER

Thermal Management Analysis for Sorbent based EVA Emergency System

2003-01-2503

View Details

X