1 of 14

Reimagining Orbital Transfer Vehicle Propulsion

“NIKOLA Y. VAPTSAROV” NAVAL ACADEMY

Engineering Faculty - Department of Electronics

A case for Rotating Detonation Engines

Created by: Emil Dimov Raychev

Internal

2 of 14

Introduction

Bridging Orbits

Spinning Fire

Taming Detonation

Ignition!

Internal

3 of 14

Bridging Orbits – What is an OTV?

Internal

4 of 14

Spinning Fire – What is a Rotating Detonation Engine?

Deflagration

Detonation

  • Up to 25% more efficient.
  • No moving parts, hence less complex.
  • More room for larger payloads.

Internal

5 of 14

Spinning Fire – What is a Rotating Detonation Engine?

 

Internal

6 of 14

DDT is not a well understood phenomenon, therefore it cannot accurately be predicted. Still,

several critical conditions need to be met before it occurs:

  1. Dimension of the tube diameter must correspond to the detonation cell size of the mixture.
  2. The shock needs to be initiated either via a pre-detonator or a spark plug.
  3. The DDT tube needs to have periodic obstacles to rapidly accelerate the flame front.
  4. CJ velocity – Needs to be around 1500 – 2500 m/s

Taming Detonation – Critical DDT Conditions

Internal

7 of 14

“For dealing with this situation, I have always recommended a good pair of running shoes.”

– John D. Clark

Taming Detonation - Fuel & Oxidizer

Criteria

Cryogenic

Hypergolic

Green

Propellant

LOX/LH₂

MMH / NTO

Specific Impulse (Isp)

420 – 450 s

300 – 330 s

290 – 320 s

Detonation ability

High

Varies

Varies

Downsides

Complexity, Boil off

Toxicity

Molecule stability

Internal

8 of 14

In order for the detonation wave to be maintained, several key factors need to be taken

into consideration:

  1. Fuel/Oxidizer injection must be axial, as opposed to radial (up to 15% better performance).
  2. Fuel/Oxidizer needs to be stored as liquid for density purposes, but vaporized prior to injection for performance.
  3. The injector plate form plays a huge part with impinging/shearing jets performing best for gas/gas systems.

Taming Detonation – Geometry

Internal

9 of 14

Rotating detonation engines need to withstand both intense pressure and heat (up to 3000K).

Some of the following materials were tested for these purposes with varying levels of success:

  1. Stainless Steel 304 🡪 Total failure. Exceeded tensile limit and melting point (1725 K).
  2. Inconel 625 🡪 Improved survivability, however melting still occurred in longer test runs.
  3. Inconel 718 🡪 Not a great heat conductor, retains a lot of the temperature.
  4. GRCop-42/GRCop-84 🡪 Higher fatigue strength, but lower thermal conductivity.
  5. CuCrZr 🡪 High thermal conductivity, but moderate tensile strength.

Taming Detonation – RDE Stability

Internal

10 of 14

Ignition! – Putting it all together

Critical DDT Conditions

Fuel & Oxidizer

Injector Geometry

RDE

Stability

Internal

11 of 14

Ignition! – Putting it all together

Internal

12 of 14

Ignition! – Putting it all together

Internal

13 of 14

What’s next?

Internal

14 of 14

Thank you for your attention!

eraychev1@gmail.com

Emil Raychev (Information Security Officer | Aspiring Space Engineer)

Internal