Military

GE combines rotating detonation and ramjet in new hypersonic engine

GE combines rotating detonation and ramjet in new hypersonic engine
The new engine will provide longer range and greater efficiency for hypersonic missiles
The new engine will provide longer range and greater efficiency for hypersonic missiles
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The new engine will provide longer range and greater efficiency for hypersonic missiles
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The new engine will provide longer range and greater efficiency for hypersonic missiles

GE Aerospace has demonstrated what it claims is the world's first hypersonic Dual-Mode Ramjet (DMRJ) rig test using Rotating Detonation Combustion (RDC) in a supersonic flow stream that could one day give hypersonic missiles longer range.

Hypersonic technology has the potential to revolutionize warfare in ways not seen since the development of supersonic flight. However, flying at over five times the speed of sound requires serious technological advances, including developing new materials and electronics that can withstand the high temperatures in the Mach 5+ realm as well as engines that can provide hypersonic vehicles with the means for sustained flight.

Currently, many hypersonic missile prototypes are what are called glide vehicles. That is, they are accelerated to a high altitude and speed, then attain hypersonic velocity by going into a dive. Only gravity and inertia from this point on provide motive power. It works, but this limits the maneuverability, range, and efficiency of the craft.

Ideally, what's wanted is an engine that can propel a missile or other craft throughout most of its flight. This would eliminate the dive phase, allow the vehicle to fly consistently at lower altitudes, increase the range, and provide more maneuverability. To do all this, the missile would need something like a ramjet engine. That's all well and good, but ramjets that can handle hypersonic conditions don't do well at low Mach numbers, so the vehicle still needs to be accelerated by a booster rocket until it's fast enough for the engine to engage.

To get around this, GE Aerospace's DMRJ uses the principle of RDC to operate at both lower and higher speeds. In RDC, fuel and air are introduced into a gap between two coaxial cylinders. When the mixture is ignited, it burns in a very special way. The combustion takes the form of a supersonic wave that travels around inside the gap. As more fuel and air are fed in at the top, the wave continues going around in the gap, producing more and more heat and pressure, and is forced down until it exits through the exit nozzle, creating thrust.

The beauty of such a ramjet design is that the design is very simple without moving parts and is suitable for hypersonic flight because it can tolerate air flowing into the chamber at supersonic speeds.

The new engine was demonstrated on a test rig at GE's Niskayuna facility in New York State. By combining the new design with the company's advances in high-temperature materials, high-temperature electronics, 3D printing, and thermal management technologies, the goal is to create a practical engine that can operate at both above Mach 5 and below Mach 3. It will also be smaller and lighter than comparable engines.

A full-scale version of the engine is expected in 2024.

"As the aerospace sector sets its sights on the future of hypersonics, GE Aerospace is well positioned with the right capabilities, experience, and scale to be a leader in driving new developments for our customers," said Amy Gowder, President and CEO, GE Aerospace, Defense & Systems. "The highly successful demonstration of a DMRJ with RDC is an outgrowth of our 10+ years of RDC work, including the strategic acquisition of Innoveering that has brought leading technologies and experience in hypersonic propulsion and ramjets."

Source: GE Aerospace

2 comments
2 comments
meofbillions
To a former researcher on liquid propellant rocket engines, the combustion described here seems to be an exploitation of something called combustion instability, in which an acoustic mode of the combustion chamber couples with energy release of the fuel/air mixture, greatly enhancing combustion rates. In this case, the acoustic mode seems to be a tangential travelling wave. My guess is that this chamber can operate without such a process, for the subsonic velocities.
jerryd
Or could just vary the ram jet nozzle with a very low cost rocket booter to start. Not sure the need for hypersonic as not economical unless near space. For weapons a lot is better than a few hypersonic which in the terminal phase gravity and a booster rocket can give that. Better would be more agility at slower speeds.