The SE2000 engine employs an oxidizer-rich staged combustion cycle, operating at a high chamber pressure of 180 bar and a specific impulse of ... class high-thrust rocket engines for future ...

The semi-cryogenic engine, powered by a combination of Liquid Oxygen (LOX) and Kerosene, delivers a high thrust of 2000 kN. It is designed to enhance the payload capacity of India's LVM3 rocket and ..

In addition to holding the propellant for its four rear-mounted rocket engines, the core is the backbone of the rocket, supporting the launch vehicle stage adapter, interim cryogenic propulsion ...

But on the Flight 8 launch preparation, they talked about saving 1 metric ton of mass per Raptor 3 engine. This must be mass beyond the engine to related components simplifications. This means about ...

VDR2 offers a single engine solution from Mach 0 to Mach 6. This marks the first successful Rocket-Based Combined Cycle test. The engine architecture was unveiled in October at UP.Summit and combines ...

Noting that these thrusters use Xenon as the propellant, the ISRO said the Specific Impulse of the Electric Propulsion System, which is a major performance indicator of a space propulsion system ...

The 10-centimeter-cube M1.5 produced thrust of 37.5 millinewtons over five minutes at a specific impulse of 4,800 seconds, while drawing power of 1.5 watts. By comparison, hydrazine propulsion ...

This rocket engine CEO faces some salacious allegations. The Independent published what it described as an exclusive report Monday describing a lawsuit filed against the CEO of RocketStar ...

The conversation with Bruno focuses on the development of the Vulcan rocket and its strategic importance. Bruno recounts the initial decision to move away from Russian RD-180 engines due to ...

in the sense that it's more or less directly correlated with the number of cores (though that doesn't mean it's true for any specific application, because they're too squidgy when it comes to ...