hypergolic propellant 3d models
24492 3d models found related to hypergolic propellant.
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
A 2:1 propellant valve-driven device is what this is termed as, which I discovered at http://www.xcor.com/gallery/main.php?g2_itemId=1140 and found it quite intriguing. ...Inspired by it, I decided to create my own unique version.
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
thingiverse
Humans utilize specialized equipment called Hakorasantacs to manage the propellant system of the cutting tool.
grabcad
54 mm class solid propellant rocket engine nozzle.Throat Diameter: 9mm
thingiverse
Rocket propellant casting base/cap for 114mm motors. This is sized for 4" PML phenolic tubing, coupler tube used for casting tube. 2 versions, one with center hole, the other 0.9" offset for moon burner. ... Core diameter is 1".
thingiverse
54mm Casting Base with center hole for 3/8″ mandrel. Sized for Snap Ring casing 54mm casting tubes. OD of the base is 1.785". Also has 1/4" hole in the base for insertion of a rod to ease removal from cast propellant.
thingiverse
... for 3/4″ mandrel. ... Sized for Snap Ring casing 75mm casting tubes. OD of the base is 2.52″. Also has 1/4″ hole in the base for insertion of a rod to ease removal from cast propellant. ... Version for both center and offset (moon burner) included.
grabcad
This project is an original idea of mine, featuring a closed-cycle gas generator. The bipropellant configuration employs liquid oxygen with RP1 as fuel. ...Distinctively, it omits pyrotechnic valves and lacks electronic components or wiring.
grabcad
This assignment serves as our last academic endeavor; it must not involve actual work, but all preparations are complete. ...If you desire the CAD files, please feel free to reach out.
thingiverse
A resealable lid for the Iams 85g cat food container is now available, as my wife couldn't find one initially; thus, I created one myself. To create this lid, print it in ABS material. ...Lightly sanding its inner edge may be necessary based on your...
grabcad
Propellant mass: 1514.00 gImpulse: 2182 NsBurn time: 1.74 sOperating pressure: 1720 psiPeak pressure: 1930 psi
thingiverse
38mm Propellant Casting Base / Cap for RCS Paper casting tubes. 1/4" center hole, print 100% infill and you can drill as needed. As there is some variation in casting tube diameters, there's a couple versions. ... One has a 1.211" OD and the other...
thingiverse
Rocket propellant casting base or cap for 29mm RCS paper tubes. 1/4" center hole, print at 100% infill and you can drill it to what you need. As there are a few versions of RCS casting tubes, there are 2 versions here. ... One with OD of 0.931"...
grabcad
The LOX-Ethanol powered engine, specifically crafted for testing purposes, has its pertinent information stored in the designated folder.
thingiverse
Combustion Lid, body and nozzle design for a bipropellant engine demands precision and attention to detail, particularly when it comes to injectors and cooling systems, which are essential for successful ignition. ...Avoid using plastic materials unless...
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...
grabcad
This is a multi-use shotgun cartridge with 9mm Luger blank fire cartridge adpoted to use instead of gunpowder&primer. Based on B&T GL-06 solution. It enables to refill the spent shells with various types of close&mid-range self-defence blunt bullets...
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.