* "/> * " />
1962-01-01

Cryogenics as Applied to the Design and Fabrication of a Space Simulation Test Cell at the Arnold Engineering Development Center * 620321

The unusual features of the Ultrahigh Altitude Rocket Cell J-2A at Arnold Engineering Development Center are described with emphasis on the cryogenic systems for cooling the diffuser and chamber liner to liquid-nitrogen temperature and the helium-refrigerated cryopumping surfaces to 20 K. It is concluded that space simulation testing of large rocket engines under actual firing conditions is possible.

SAE MOBILUS

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

Access SAE MOBILUS »

Members save up to 18% 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.
X