admin
09-03-2005, 08:17 AM
Technical Details
Payload (kg)760-987-1,158
(satellite or warhead)
Range (km)>1,500
CEP (m)190
(previously thought to be
several thousand meters)
Stages2Diam. (m)1.32-1.35-1.85
Height (m)~17.1
L. W. (kg)~16,500/unknown
TypeMRBM
Sounding Research Rocket
2nd & 3rd stages of a space booster or LRBM
Stage 1Height (m)~14
Diameter (m)1.32-1.35-1.85
Mass (kg)15,092
D.W (kg)2,180-1,780
Thrust (Kg f)Effective: 26,051 (-709)
Actual: 26,760-26,600
Burn Time (sec.)110
Isp. (sec.)Effective: 226 - SL
Due to vanes steering drag loss of 4-5 sec.
Actual: 230 - SL
Vac: 264
Thrust Chambers1
FuelTM-185
(20% Gasoline + 80% Kerosene)
OxidizerAK-27I
(27% N2O4 + 73% HNO3 + Iodium Inhibitor)
Propellant Mass (kg)12,912
Stage 2*Height (m)~3-4 total package
Diameter (m)~1.3-2.0 flared skirt type design
Launch Weight (kg)unknown
Launch Thrust (kg f)unknown
Burn Time (sec.)~100
PropellantSolid propellant
Payload (kg)760-987-1,158
(satellite or warhead)
Range (km)>1,500
CEP (m)190
(previously thought to be
several thousand meters)
Stages2Diam. (m)1.32-1.35-1.85
Height (m)~17.1
L. W. (kg)~16,500/unknown
TypeMRBM
Sounding Research Rocket
2nd & 3rd stages of a space booster or LRBM
Stage 1Height (m)~14
Diameter (m)1.32-1.35-1.85
Mass (kg)15,092
D.W (kg)2,180-1,780
Thrust (Kg f)Effective: 26,051 (-709)
Actual: 26,760-26,600
Burn Time (sec.)110
Isp. (sec.)Effective: 226 - SL
Due to vanes steering drag loss of 4-5 sec.
Actual: 230 - SL
Vac: 264
Thrust Chambers1
FuelTM-185
(20% Gasoline + 80% Kerosene)
OxidizerAK-27I
(27% N2O4 + 73% HNO3 + Iodium Inhibitor)
Propellant Mass (kg)12,912
Stage 2*Height (m)~3-4 total package
Diameter (m)~1.3-2.0 flared skirt type design
Launch Weight (kg)unknown
Launch Thrust (kg f)unknown
Burn Time (sec.)~100
PropellantSolid propellant