Nitrogen Tetroxide & Aerozine 50*
* 50% UDMH + 50% N
2
H
4
Adiabatic Flame Temperature
Gas Molecular Weight
Specific Heat Ratio
Home Page
Basics of Space Flight
- Rocket Propellants
- Rocket Propulsion
- Orbital Mechanics
- Interplanetary Flight
Space Hardware
- Spacecraft Systems
- Vehicle Specifications
- Space Launch Vehicles
Space Missions
- Manned Space Flights
- Planetary Spacecraft
- Lunar Spacecraft
World Space Centers
Space Milestones
Glossary
Bibliography
Home
