SOLVED: A liquid propellant rocket uses hydrazine for fuel and NO4 for oxidizer. The rate of hydrazine injection is 4 g/s and that of NO4 is 6 g/s. If the mean diameter of hydrazine and NO4 droplets formed in the spray is 0.3 mm and the mean axial velocity of droplets is 50 m/s, determine:i. Mixture ratio at injectionii. Mixture ratio of the vaporized propellantYou can take the length of the combustion chamber as 50 cm. The evaporation of the droplets can be assumed to be given by the law: d = d

The space shuttle Orbiter uses the oxidation of methyl hydrazine by dinitrogen tetroxide for propulsion: 5 N2 O4(g) 4 N2 H3 CH3(g) → 12 H2 O(g) 9 N2(g) 4 CO2(g) Use bond energies to estimate ΔH for this reaction. The structures for the reactants are | Numerade

Hydrazine Hydrate Chemical

Catalysed Hydrazine Hydrate

Hydrazine Dihydrochloride

aniline to phenyl hydrazine? - c566pfpp

Vintage Air Force Video Explains F-16 Fighting Falcon's EPU Hydrazine Hazards

Hydrazine Hydrate 80

Hydrazine Hydrate 80%