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Contents

   



(Top)
 


1 Description  





2 Applications  





3 Specifications  



3.1  General characteristics  





3.2  Components  





3.3  Performance  







4 See also  





5 Notes  





6 External links  














Walter HWK 109-500






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From Wikipedia, the free encyclopedia
 


HWK 109-500
HWK 109-500 on display at the Royal Air Force Museum Cosford
Type Liquid-propellant rocket (assist unit)
Manufacturer Hellmuth Walter Kommanditgesellschaft
Number built 6,000
Walter 109-500 on display

The Walter HWK 109-500 was a liquid-fuelled rocket engine developed by WalterinGermany during the Second World War.

Description[edit]

The 109-500 is a self-contained, modular monopropellant Starthilfe (take-off assist) engine in a pod, able to produce 500 kg (1,100 lb) thrust for thirty seconds. After the fuel was expended, the pod was jettisoned and it returned to earth by parachute,[1] with the parachute packed externally, onto the blunt forward end of the pod.

The T-Stoff monopropellant, stored in the large spherical tank within the Starthilfe module's forward end, needed to react with a catalyst to provide the boosting thrust for an aircraft on takeoff - this Z-Stoff sodiumorcalcium-based, alkaline permanganate-compound (in an aqueous solution) catalyst was provided in a small tank above the reaction chamber just forward of the exhaust nozzle, with compressed air from a network of five pressure tanks driving the monopropellant and catalyst together through the reaction chamber, which featured an internal, fixed helical "swirl baffle" to lengthen the period of time the monopropellant and catalyst were in contact for a more complete catalytic reaction within it, before the reacted T-Stoff exhaust exited the nozzle.[2]

It entered service in 1942, and some 6,000 were built, by Heinkel.[1] It was "used extensively on a wide range of aircraft", especially the potentially underpowered (when heavily laden with external ordnance) Jumo 004-engined Arado Ar 234B,[1] with two of the units uniquely displayed as mounted operationally on the NASM's sole surviving, restored Ar 234B.

Applications[edit]

Specifications[edit]

Data from The race for Hitler's X-planes : Britain's 1945 mission to capture secret Luftwaffe technology,[1] Die Deutsche Luftruestung 1933–1945 Vol.4 – Flugzeugtypen MIAG-Zeppelin[3]

General characteristics

Components

Performance

See also[edit]

Related lists

Notes[edit]

  1. ^ a b c d Christopher, John (2012). The race for Hitler's X-planes : Britain's 1945 mission to capture secret Luftwaffe technology. Stroud: History. p. 125. ISBN 978-0752464572.
  • ^ Reddin, Shamus. "Walter HWK 109-500 RI-201: "Cold" Rocket Assisted Take-Off Pack". walterwerke.co. Retrieved 16 March 2018.
  • ^ Nowarra, Heinz J. (1993). Die Deutsche Luftruestung 1933–1945 Vol.4 – Flugzeugtypen MIAG-Zeppelin (in German). Koblenz: Bernard & Graefe Verlag. pp. 121, 124. ISBN 3-7637-5468-7.
  • External links[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Walter_HWK_109-500&oldid=1037714800"

    Categories: 
    Aircraft rocket engines
    HWK rocket engines
    JATO
    Rocket engines using cold cycle hydrogen peroxide propellant
    Hidden categories: 
    CS1 German-language sources (de)
    Articles with short description
    Short description matches Wikidata
    Commons category link is on Wikidata
    Aircraft engines without specifications
     



    This page was last edited on 8 August 2021, at 07:57 (UTC).

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