RD-0221
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RD-0221
Credit - © Dietrich Haeseler
Engine Model
: RD-0221.
Manufacturer Name
: RD-0221.
Designer
: Kosberg.
Developed in
: 1965-70.
Application
: upper stage of unnamed missile by Mishin.
Propellants
: N2O4/UDMH.
Thrust(vac)
: 78.000 kN (17,535 lbf).
Isp
: 330 sec.
Isp (sea level)
: 300 sec.
Burn time
: 800 sec.
Mass Engine
: 150 kg (330 lb).
Diameter
: 0.80 m (2.62 ft).
Length
: 1.60 m (5.20 ft).
Chambers
: 1 + 2.
Chamber Pressure
: 122.60 bar.
Thrust to Weight Ratio
: 53.02.
Country
: Russia.
Status
: Developed 1965-70.
Bibliography:
Haeseler, Dietrich, Visit to the museum of Chemical Automatics Design Bureau, Voronezh 1992 via Dietrich Haeseler.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
