RD-0108
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RD-0110 Engine
Credit - © Mark Wade
Engine Model
: RD-0108.
Manufacturer Name
: RD-0108.
Government Designation
: 8D715P.
Other Designations
: RD-461, 11D55, 8D715K, RO-8.
Designer
: Kosberg.
Developed in
: 1961-65.
Application
: Voskhod 11A57, Molniya 8K78 stage 3.
Propellants
: Lox/Kerosene.
Thrust(vac)
: 297.900 kN (66,971 lbf).
Isp
: 326 sec.
Burn time
: 250 sec.
Mass Engine
: 410 kg (900 lb).
Diameter
: 0.64 m (2.09 ft).
Chambers
: 4.
Chamber Pressure
: 68.20 bar.
Thrust to Weight Ratio
: 74.09.
Country
: Russia.
First Flight
: 1960.
Last Flight
: 1976.
Flown
: 326.
RD-0108 used on Rocket Stages
Used on stage
:
Soyuz Block I
.
on launch vehicle
:
Angara
.
Used on stage
:
Soyuz Block I
.
on launch vehicle
:
GR-1
.
Used on stage
:
Soyuz Block I
.
on launch vehicle
:
R-9
.
Used on stage
:
Soyuz Block I
.
on launch vehicle
:
Soyuz
.
Bibliography:
Varfolomyev, Timothy,
Spaceflight
, "Soviet Rocketry that Conquered Space - 8K71 launches", 1996, Volume 38, page 31.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
