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Kartukov Soyuz T - TM SAS 17k
Designer
: Kartukov.
Developed in
: -1979.
Application
: Soyuz T, Soyuz TM.
Used on spacecraft
:
Soyuz T
,
Soyuz TM
. Propellants:
Solid
Thrust(vac)
: 17,500 kgf.
Thrust(vac)
: 171.00 kN.
Country
: Russia.
Status
: In Production.
Comments
: Thrust 10 tf at cutout - 17.5 at ignition.
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Last update 12 March 2001.
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© Mark Wade, 2001 .