Walter HWK 109-509

Walter HWK 109-509

The HWK 109-509 was a German liquid-fuel bipropellant rocket engine that powered Messerschmitt Me 163 and Bachem Ba 349 aircraft. It was produced by Hellmuth Walter Kommanditgesellschaft.

It used a two component hypergolic fuel/oxidizer combination, controlled by two pumps, to regulate the rate of combustion and thereby the amount of thrust. The engine worked on the principle of the "hot" Walter drive which used T-Stoff in place of Z-Stoff, the latter tending to clog the jets in the combustion chamber, causing fluctuations in power and potentially explosions.

The fuel was known as C-Stoff, a mix of 30 % hydrazinhydrat + 57 % methanol + 13 % water with a small amount of potassium-copper-cyanide, and the oxidizer, known as T-Stoff, consisted of a hydrogen peroxide which reacted violently on contact, as a hypergolic propellant combination. [Botho Stüwe, Peene Münde West, Weltbildverlag ISBN 3-8289-0294-4 1998 page 220, German] The violent combustion process resulted in the formation of water, carbon dioxide and nitrogen, and a huge amount of heat sending out a superheated stream of steam, nitrogen and air that was drawn in through the hole in the mantle of the engine, thus providing a forward thrust of approximately 17 kN (3,800 lbf).

The engine was an integral design with all components of the drive, with the exception of fuel tanks, locked in a frame.

Versions

*"A-0": Pre-production model, manufactured from May 1943. The thrust of this engine was regulated between 300 kp (2.9 kN) and 1500 kp (14.7 kN).
*"A-1": The first series production engine was used in the Messerschmitt Me 163 B from August 1944. The thrust here was adjustable between 100 kp (1 kN) and 1600 kp (15.7 kN).
*"A-2": version for the Messerschmitt Me 163B-1a. Weighing only 100kg complete, this engine consisted of two main assemblies, the forward assembly comprising the turbine housing, the fuel pumps geared to the turbine shaft, the control box, a pressure-reducing valve and the electric starter motor, with the aft assembly made up of the combustion chamber, connected to the fore unit by a cylindrical tube containing pipes which carried fuel to the individual jets. The thrust was adjustable between 200 kp (2 kN) to a maximum of 1700 kp (16.7 kN).
*"B-1": Increased performance version of the A-1. This engine had a cruising combustion chamber just below the main combustion chamber, with an additional thrust of 300 kp (2.9 kN). This auxiliary chamber proved necessary due to the actual T-Stoff consumption of the main unit exceeding calculated estimates by 100% at nearly 5kg/s.Thrust adjustable between 100 kp (1 kN) and 2000 kp (19.6 kN).
*"C-1": Based on the uprated version of the A-2. The main combustion chamber gave between 400 kp (3.9 kN) and 2000 kp (19.6 kN), auxiliary chamber 400 kp (3.9 kN). To be used in the Me 263 and Ju 248.
*"D-1": variant of the C-1 for use in the Bachem Ba 349. Designed to be parachute-dropped.

References


Wikimedia Foundation. 2010.

Игры ⚽ Нужно решить контрольную?

Look at other dictionaries:

  • Walter HWK 109-509 — HWK 109 509 HWK 109 509 expuesto en el Luftwaffenmuseum, Berlín Gatow (Alemania). Tipo Motor cohete Fabricante …   Wikipedia Español

  • Walter HWK 109-509 — Die Walter HWK 109 509 war ein Flüssigkeitsraketenantrieb im Zweiten Weltkrieg. Der Antrieb wurde unter anderem in der Messerschmitt Me 163 und der Bachem Ba 349 eingesetzt. Die Basis bildete das zuvor entwickelte Walter R 1 203. Das Triebwerk… …   Deutsch Wikipedia

  • Walter R 1-203 — Das Walter R 1 203 war ein Flüssigkeitsraketentriebwerk des deutschen Erfinders Hellmuth Walter. Entwickelt wurde es 1938 als Versuchstriebwerk. Es basiert auf dem heißem Walter Antrieb. Demzufolge fand eine Verbrennung in der Brennkammer statt.… …   Deutsch Wikipedia

  • Hellmuth Walter Kommanditgesellschaft — (HWK), commonly known as the Walter Werke, was a German company founded by Professor Hellmuth Walter to pursue his interest in engines using hydrogen peroxide as a fuel.Having experimented with torpedoes and submarines, Walter began to design… …   Wikipedia

  • Hellmuth Walter — (26 August 1900 in Wedel near Hamburg – 16 December 1980 in Upper Montclair, New Jersey) was a German engineer who pioneered research into rocket engines and gas turbines. His most noteworthy contributions were rocket motors for the Messerschmitt …   Wikipedia

  • Messerschmitt Me 163 — Not to be confused with Messerschmitt Bf 163. Me 163 Komet Me 163B 1a at the National Museum of Flight in Scotland …   Wikipedia

  • List of aircraft engines — ABC Dragonfly at the London Science Museum This is an alphabetical list of aircraft engines by manufacturer. Contents A B …   Wikipedia

  • Ba 349 — Bachem Ba 349 Natter auf der Kriegsbeuteschau 1946 in Farnborough (England). Die Hakenkreuze wurden von den Briten ohne realen Bezug nachträglich aufgemalt …   Deutsch Wikipedia

  • Bachem Ba 349 Natter — auf der Kriegsbeuteschau 1946 in Farnborough (England). Die Hakenkreuze wurden von den Briten ohne realen Bezug nachträglich aufgemalt …   Deutsch Wikipedia

  • Bachem Natter — Bachem Ba 349 Natter auf der Kriegsbeuteschau 1946 in Farnborough (England). Die Hakenkreuze wurden von den Briten ohne realen Bezug nachträglich aufgemalt …   Deutsch Wikipedia

Share the article and excerpts

Direct link
Do a right-click on the link above
and select “Copy Link”