John C. Stennis Space Center provides rocket engine propulsion testing for the NASA space programs. Since the development of the Space Shuttle, every Space Shuttle Main Engine (SSME) has gone through acceptance testing before going to Kennedy Space Center for integration into the Space Shuttle. The SSME is a large cryogenic rocket engine that uses Liquid Oxygen (LO2) and Liquid Hydrogen (LH2) as propellants. Due to the extremely cold cryogenic conditions of this environment, an inert gas, helium, is used as a purge for the engine and propellant lines since it can be used without freezing in the cryogenic environment.

High Pressure Gas Facility (HPGF) – GN, GHe, GH, Air
As NASA moves forward with the development of the new ARES V launch system, the main engines as well as the upper stage engine will use cryogenic propellants and will require gaseous helium during the development testing of each of these engines. The main engine for the ARES V will be similar in size to the SSME.

Technology Needs

Due to the size of the SSME and the test facilities required to test the engine, extremely large quantities of helium are used during testing each year. This requirement makes Stennis one of the world’s largest users of gaseous helium, which is a non-renewable natural resource. The cost of helium is increasing as the supply diminishes, and it is beginning to impact testing of the rocket engines for space propulsion systems.

Innovative solutions are needed for efficient and cost-effective methods to measure hydrogen concentrations in a helium background during the engine purging and testing processes. By better understanding when the purging process is complete, helium gas usage can be reduced significantly. Research into technologies in these areas, demonstration of the technology capability, and conceptual design for the technology installation at Stennis are desired to assist in helium use reduction.

Technology Challenges

High Pressure Gas Facility (HPGF) – GN, GHe, GH, Air
Helium is used in piping and engine purge processes to inert liquid hydrogen systems. Because of this, hydrogen-inhelium concentration devices must stand up to this severe cryogenic temperature condition. One of the challenges will be to develop a measurement device that detects small amounts of hydrogen in a helium background while surviving in this environment. In order to allow more and faster data to be collected from the device, another challenge will be the development of a system that can be used to detect hydrogen in a helium background continuously without the use of a vacuum system to test a small sample.

The technologies developed to detect hydrogen concentrations in a helium background must be cost effective and able to perform in a cryogenic temperature environment. Such technologies will be required to comply with all safety and quality standards required in this environment.

More Information

For additional information, or to discuss ideas about this, contact John Lansaw at 228-688-1962 or This email address is being protected from spambots. You need JavaScript enabled to view it., or visit This email address is being protected from spambots. You need JavaScript enabled to view it..

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