Aircraft

Rotating detonation ramjet engine for hypersonic speeds to fly in 2025

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Render of a passenger airliner equipped with VDR2 engines
Venus Aerospace
Render of a passenger airliner equipped with VDR2 engines
Venus Aerospace
A cutaway view of the VDR2
Venus Aerospace

When is an empty tube not an empty tube? When it's a ramjet that uses rotating detonation technology to propel aircraft at hypersonic speeds. A case in point is Venus Aerospace's new Venus Detonation Ramjet 2000 lb Thrust Engine (VDR2).

One of the biggest hurdles that need to be cleared in making hypersonic flight practical is building engines that are capable of sustained thrust.

Currently, hypersonic systems are mainly based on glide bodies that are boosted to high speed and altitude by rockets and then accelerate to over Mach 5 by gliding back to lower altitudes. However, if you want to build airliners that can fly from San Francisco to Tokyo in one hour, you need something more like a jet engine.

Unveiled at the recent Up.Summit in Bentonville, Arkansas the VDR2 looks ridiculously simple in a cutaway view because it's essentially an empty tube without moving parts. This is because it's mainly a ramjet, where the incoming air is compressed by the speed of the engine moving forward instead of by spinning turbine blades as in a conventional jet engine.

The reason a ramjet is attractive for hypersonic flight is that it can tolerate much higher temperatures than a conventional engine thanks to being mechanically simple and having no moving parts. This is important because air coming into an engine at hypersonic speeds can make the interior reach 2,130 °C (3,860 °F) and would quickly melt turbine blades or similar components.

However, there is room for improvement. The VDR2 takes things a step further by incorporating a Rotating Detonation Rocket Engine (RDRE), which overcomes the limitations of a rocket or jet engine by using another novel principle – again, with no moving parts. The RDRE part of the VDR2 consists of two coaxial cylinders with a gap between them. A fuel/oxidizer mixture is squirted into the gap and ignited. The next step is a bit tricky, but if the detonation is configured properly, this generates a closely coupled reaction and shock wave that speeds around inside the gap at supersonic velocity that generates more heat and pressure.

A cutaway view of the VDR2
Venus Aerospace

The result is a low-drag engine being developed in partnership with Velontra and builds on a previous Venus Aerospace project. It has the high thrust and efficiency needed to power an aircraft to speeds of up to Mach 6 and an altitude of 170,000 ft (52,000 m) and is 15% more efficient than conventional engines, if Venus Aerospace meets its current design goals.

"This engine makes the hypersonic economy a reality," said Venus Aerspace CTO Andrew Duggleby. "We are excited to partner with Velontra to achieve this revolution in high speed flight, given their expertise in high-speed air combustion."

The VDR2 is expected to make its first test flight in a test drone next year.

Source: Venus Aerospace

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7 comments
windykites
Who needs to get anywhere that quickly? I bet the engine is loud! Also it looks like a fuel gulper!
Steve7734
how does it get up to speed so the RDE can get going? Or does it work from a stand-still?
Mike Vidal
Windykites, it sounds as if you’ve never done the 12 to 14 hour flights to Asia
Nelson
Do rich people really need to destroy the environment so they can get to their possesions around the world faster?
Nelson
Mike Vida, and unless you are crazy rich you will never get to Asia any faster.
Wavmakr
Anyone see a slight resemblance to the SR71 Blackbird….?
rgbatduke
Getting to 52 km up at 2 km/sec (give or take) still leaves one 6 km/sec short of a circular orbit, but very likely in a nice ballistic trajectory and certainly out of MOST of the atmosphere. This could conceivably be used as a first stage for an orbital launch vehicle with the advantage that it doesn't have to carry oxidizer for the first stage fuel it uses through the high-drag part of the atmosphere before turning on real rockets while in ballistic flight to get the rest of the boost into orbit. Because of the huge "rocket fuel" penalty (lifting the fuel to lift the fuel to lift the fuel to lift the fuel.... to lift the rocket payload) saving on oxidizer could conceivably make orbital launches MUCH cheaper.

Obviously, it's also great as a basis for hypersonic missiles and missile defense systems, where the transition to a second stage boost is not needed. At 2 km/sec, a warhead boosted in this way to 52 km should have an impressive free/ballistic range, and the booster could be designed to separate and come down gently for reuse.