hypergolic 3d models
9 3d models found related to hypergolic.
grabcad
As a Solidworks newbie, I created an engine design for the first time using 4130 Steel or SUS304 plated with Copper-Nickel-Chromium. The open-source model is available for download and modification at no cost. ...If you detect any errors, kindly correct...
grabcad
Oxidizer: 98% nitric acidFuel: amine50Oxidizer - Fuel flow ratio: 4.5Chamber pressure: 5 MpaChamber Temperature: 3185 KPressure-fed cycle: 7.5 MpaInjection chamber pressure: 6 Mpa
sketchfab
Hypergolic fuel, a liquid propellant, is highly toxic, and is handled under the most stringent safety conditions. This building was constructed to provide storage for the hazardous protective clothing needed by workers. ...See also:...
thingiverse
... to replace the more expensive M-V rocket. Epsilon consists of a booster from the H-II rocket, and upper stages from the Mu family of rockets. All 3 stages are solid fuel with the option of a 4th hypergolic liquid fuel stage. ... Scale 1:100
thingiverse
... and 1.35 meters in diameter. It has a solid fuel first, second, and third stage with a small hypergolic fourth stage. It's most notable for its retrograde launches due to conflicts with neighbors to the east of the nation. ...Model at 1:100 scale.
thingiverse
The Proton-M launch vehicle consists of three stages; all of them powered by liquid rocket engines using the hypergolic propellant combination of dinitrogen tetroxide as the oxidizer, and unsymmetrical dimethylhydrazine for fuel. The vehicle does not...
cgtrader
The R-4D is a small hypergolic rocket engine, originally designed by Marquardt Corporation for use as a reaction control thruster on vehicles of the Apollo moon program. The engine runs on self-igniting components: monomethylhydrazine and nitrogen...
cgtrader
It was a liquid fuel rocket using a hypergolic combination of unsymmetrical dimethylhydrazine (UDMH) as fuel, and nitrogen tetroxide (NTO) as oxidizer.[1] Between 1974 and 1990, 161 missile launches were conducted, with an average success rate of...
thingiverse
... from the Soviet Proton rocket. This launch vehicle consists of three stages, all powered by liquid-fueled engines running on the hypergolic propellant combination of dinitrogen tetroxide as the oxidizer and unsymmetrical dimethylhydrazine as fuel.