1940s German aircraft rocket engine
The BMW 109-558 is a liquid fuelled sustainer rocket motor developed by BMW at their Bruckmühl facility,[ 1] 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)[ 2] was designed as a sustainer rocket for the Henschel Hs 117 surface-to-air missile .[ 3] It was tubular, measuring 12.5 cm (4.9 in) diameter and about 46 cm (18 in) long overall.[ 4] 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 ).[ 5] SV-Stoff was used to cool the combustion chamber.[ 6]
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.[citation needed ]
Applications
Specifications
General characteristics
Components
Notes
^ Christopher, John. The Race for Hitler's X-Planes (The Mill, Gloucestershire: History Press, 2013), p.127.
^ Christopher, p.124.
^ Christopher, p.127.
^ Christopher, p.127.
^ Christopher, p.127.
^ Christopher, p.127.
^ Christopher, p.127.
Sources
Christopher, John. The Race for Hitler's X-Planes . The Mill, Gloucestershire: History Press, 2013.
Liquid fuel
Cryogenic
Hydrolox (LH2 / LOX )
China
Europe
India
Japan
Russia
United States
Methalox (CH4 / LOX )
China
United States
Russia
Europe
Semi- cryogenic
Kerolox (RP-1 / LOX )
China
India
Russia
NK-15
NK-33, 44
RD-58
RD-0105, 0109
RD-0107, 0108, 0110
RD-0110R
RD-0124
RD-107, 108, 117, 118
RD-120
RD-170, 171
RD-180
RD-191, 151, 181
RD-193
S1.5400
Spain
Ukraine
United States
Storable
Hypergolic (Aerozine , UH 25 , MMH , or UDMH / N2 O4 , MON , or HNO3 )
China
Europe
India
Israel
North Korea
Russia
17D61
RD-0202 to 0206, 0208 to 0213
RD-0207, 0214
RD-0216, 0217, 0235
RD-0233, 0234
RD-0236
RD-0237
RD-0243 to 0245
RD-0255 to 0257
RD-215 to 219
RD-250 to 252, 261, 262
RD-253, 275
RD-263, 268, 273
RD-270
S5.92
S5.98M
Ukraine
United States
Other
Solid fuel
China
Europe
India
Iran
Israel
Japan
United States
* Different versions of the engine use different propellant combinations
Engines in italics are under development