A Cryogenic Breathing Apparatus; Its Operation And Use

Approximately forty years ago, the military services began a realistic investigation of the problems involved with the replacement of high pressure gaseous systems with liquid oxygen systems. The program was temporarily discontinued because of numerous State-of-the-Art problems. Ten years later, interest in the liquid oxygen breathing concept was revived. Initial testing of this concept was completed in 1946. The ensuing years have seen the general acceptance of many cryogenic breathing systems for airborne applications. The inherent features of weight savings (approximately 70%) and space savings (approximately 80%) make it very desirable for high performance military aircraft. A typical aircraft system consists of a storage container with appropriate integrated control valving (the liquid oxygen converter), a heat exchanger, breathing regulator, and oxygen mask. Normally the liquid converter is located in the aircraft wheel well for easy access by ground crew personnel and the breathing regulator is mounted in the cockpit where the pilot can connect his oxygen mask. An aircraft system such as this will provide the pilot with eight hours of breathing oxygen after a 24 hour standby period. Early in 1960, the National Aeronautics and Space Administration sought a means of providing a cooling system for their personnel involved in fueling the rockets used in the space program. While fueling rockets N.A,S.A, personnel wore a completely enclosed butyl rubber suit and were susceptible to heat prostration. Using the concept of an aircraft system, Aro redesigned the container, heat