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Kartukov Soyuz T - TM SAS 73k
Designer
: Kartukov.
Developed in
: -1979.
Application
: Soyuz T, Soyuz TM.
Used on spacecraft
:
Soyuz T
,
Soyuz TM
. Propellants:
Solid
Thrust(vac)
: 73,000 kgf.
Thrust(vac)
: 715.00 kN.
Country
: Russia.
Status
: In Production.
Comments
: Thrust 45 tf at cutout - 73 tf at ignition.
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Last update 12 March 2001.
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© Mark Wade, 2001 .