hypergolic 3d models

I am a novice in Solidworks, and I designed this engine for the first time.Material: 4130 Steel or SUS304 plated with Copper-Nickel-Chromium.This model is completely open-source, you can download and edit the files for free.If you find some incorrect...

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

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:...

... 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

... 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.

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...

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...

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...

... rocket. 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. ...

Korolev was an outspoken opponent of hypergolic propellants due to their toxicity, often citing the 1960 Nedelin catastrophe as evidence of the danger posed by them, and had also objected to the UR-500 for the same reason. Glushko meanwhile was an...