Dushkin S-155

Dushkin S-155
S-155
Country of origin Soviet Union
Manufacturer Dushkin OKB
Application Booster rocket for aircraft
Liquid-fueled engine
Propellant AK-20 (nitric acid) / TG-02 hypergolic kerosene
Performance
Thrust (SL) 37.3 kN (8380 lbf)

The Dushkin S-155 was a liquid-fueled rocket motor designed by Leonid Dushkin specifically for use in the Mikoyan-Gurevich Ye-50 and Ye-50A (aka MiG-23U) experimental-developmental aircraft in the 1950s. It delivered 37.3 kN (8380 lbf) and ran on a mix of TG-02 hypergolic kerosene and AK-20 oxidizer (nitric acid). The fuel pumps were powered with grade T hydrogen peroxide. [1]

References

  1. ^ Gordon, Yefim "MiG-21" ISBN 978-1-85780-257-3
v · d · eFlown rocket engines and rocket motors
Liquid fuel
US
J-2 · RL10 · RL60 · RS-68 · SSME · M-1
EU
HM7B · Vinci · Vulcain
Russia
RD-0120 · RD-0146
Japan
India
CE-15 · CE-20
China
YF-50t · YF-73 · YF-75 · YF-77 · YF-100
Semi-Cryogenic

(RP-1/LOX)
US
F-1 · H-1 · Kestrel · Merlin · RS-27A
EU
Russia
NK-33 · RD-0124 · RD-107  · RD-117 · RD-120 · RD-170 · RD-180 · RD-191 · RD-58 · RD-8
China
YF-100 · YF-120t
Hypergolic
RD-253 · RD-270 · Vikas engine
RP-1/H2O2
other
Dushkin S-155 · Walter HWK 109-509
RS-68 rocket engine test.jpg
Solid fuel
Star 48 · P230 · Space Shuttle Solid Rocket Booster · 1.5KS35000 · 1.8KS7800 · 1.9KS2150 · Jetex engine · Waxwing
Nuclear Thermal/Electric
NERVA · RD-0410 · 11B97

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