"The J-2 Liquid Hydrogen Rocket Engine."
The 5-2 high-energy liquid propellant rocket engine (~i~. l), a large engine producing 200,000 pounds of thrust at altitude conditions, burns liquid hydrogen and liquid oxygen to produce the necessary high specific impulse for practical space use. Rocketdyne, a Division of North American Aviation, I...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Electronic |
| Published: |
University of Alabama in Huntsville Archives
|
| Subjects: | |
| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10924 |