Effect of additives on the ignition delay time of hypergolic propellants.
Additives effect on ignition delay and pressure of hypergolic hydrazine-nitrogen tetroxide propellant systems.
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Additives effect on ignition delay and pressure of hypergolic hydrazine-nitrogen tetroxide propellant systems.
Ablative material degradation in liquid propellant rocket engine environment of nitrogen tetroxide-aerozine
Injector baffles for flame stability in combustion chambers using nitrogen tetroxide and hydrazine mixture
Exhaust gas of hydrazine-nitrogen tetroxide rocket for simulating combustor inlet requirements of scramjet engines
Mechanism and design parameter effects in stream mixing and separation of nitrogen tetroxide-hydrazine impingement
Preignition phenomena in small Aerozine-50/ nitrogen tetroxide pulsed rocket engines shown partly due to hydrazine nitrate accumulation
Azides and hydrazoic acid formation as intermediates involved with pressure spiking when restarting nitrogen tetroxide-hydrazine engines in vacuum
Measurement of heat release rate for liquid phase reaction of nitrogen tetroxide and hydrazine
Liquid hydrazine ignition by nitrogen tetroxide gas based on stagnation flow principle, presenting threshold measurements
Ball valve design incorporates modular construction in easy-to-install, easy-to-replace cartridge housing, and a system of cams to lift upstream and downstream seals away from the ball during rotation. Tests conducted on nitrogen tetroxide prove new valve to be more efficient than previous models in preventing leakage.
Boundary flow chemical composition and heat flux data from hydrazine-nitrogen tetroxide rocket engine - Part 1
Tungsten-rhenium alloy thermocouples to determine distribution of hydrazine-nitrogen tetroxide products within combustion chamber
Stress corrosion cracking susceptibility of titanium alloys in nitrogen tetroxide and aqueous and hot salt environments
Fracture and sustained load flaw growth characteristics for titanium alloy evaluated in nitrogen tetroxide
Nitrogen tetroxide resistant positive propellant expulsion bladder for Saturn 5/S-4B stage made of electroformed gold and rubber laminate
Operating fuel cells on gaseous nitrogen tetroxide and aerozine 50
Optimum penetration and separation mixing of unlike doublet injector element with hypergolic hydrazine and nitrogen tetroxide propellants
Reactive stream separation high speed color photography for impinging streams of nitrogen tetroxide and hydrazine