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About: BMW 109-558

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The BMW 109-558 is a liquid fuelled sustainer rocket motor developed by BMW at their Bruckmühl facility, in Germany during the Second World War. The 109-558 (with the "109-" prefix being the Reichsluftfahrtministerium, or RLM, designation for reaction-propulsion aircraft power projects, encompassing all jet & rocket engine designs) was designed as a sustainer rocket for the Henschel Hs 117 surface-to-air missile. It was tubular, measuring 12.5 cm (4.9 in) diameter and about 46 cm (18 in) long overall. The engine had a compressed air tank to pressurise tanks for the R-Stoff fuel (50% triethylamine and 50% xylidine) and SV-Stoff oxidiser (94% nitric acid with 6% dinitrogen tetroxide). SV-Stoff was used to cool the combustion chamber.

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dbo:abstract
  • The BMW 109-558 is a liquid fuelled sustainer rocket motor developed by BMW at their Bruckmühl facility, in Germany during the Second World War. The 109-558 (with the "109-" prefix being the Reichsluftfahrtministerium, or RLM, designation for reaction-propulsion aircraft power projects, encompassing all jet & rocket engine designs) was designed as a sustainer rocket for the Henschel Hs 117 surface-to-air missile. It was tubular, measuring 12.5 cm (4.9 in) diameter and about 46 cm (18 in) long overall. The engine had a compressed air tank to pressurise tanks for the R-Stoff fuel (50% triethylamine and 50% xylidine) and SV-Stoff oxidiser (94% nitric acid with 6% dinitrogen tetroxide). SV-Stoff was used to cool the combustion chamber. The 109-558 was capable of propelling an Hs 117 at 900–1,000 km/h (560–620 mph; 490–540 kn), with throttle control by sliding valves in the exhaust nozzle, operated by a servomotor controlled by a Mach sensor. Production of the 109-558 took forty to sixty hours using a very high proportion of slave labour. (en)
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  • 42969315 (xsd:integer)
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  • 3716 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1103359958 (xsd:integer)
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dbp:combustion
  • Hypergolic combustion in a single combustion chamber (en)
dbp:fueltype
  • R-Stoff fuel and SV-Stoff oxidiser (en)
dbp:majorApplications
  • Henschel Hs 117 Schmetterling missile (en)
dbp:manufacturer
dbp:nationalOrigin
dbp:numberBuilt
  • 120 (xsd:integer)
dbp:thrust
  • 24.0 (dbd:second)
dbp:thrust/weight
  • 0.023125 (xsd:double)
dbp:type
dbp:unitCost
  • 400 (xsd:integer)
dbp:weight
  • . (en)
dbp:wikiPageUsesTemplate
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rdfs:comment
  • The BMW 109-558 is a liquid fuelled sustainer rocket motor developed by BMW at their Bruckmühl facility, in Germany during the Second World War. The 109-558 (with the "109-" prefix being the Reichsluftfahrtministerium, or RLM, designation for reaction-propulsion aircraft power projects, encompassing all jet & rocket engine designs) was designed as a sustainer rocket for the Henschel Hs 117 surface-to-air missile. It was tubular, measuring 12.5 cm (4.9 in) diameter and about 46 cm (18 in) long overall. The engine had a compressed air tank to pressurise tanks for the R-Stoff fuel (50% triethylamine and 50% xylidine) and SV-Stoff oxidiser (94% nitric acid with 6% dinitrogen tetroxide). SV-Stoff was used to cool the combustion chamber. (en)
rdfs:label
  • BMW 109-558 (en)
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