Taep'o-dong 2 (TD-2)
Technical Details
Payload (kg) 100-500
700-1,000
Range (km) 3,500-4,300 (2-stages)
4,000-4,300 (3-stages)
CEP (m) unknown
Diam. (m) 2.2/1.3
Height (m) 32
L. W. (kg) 80-85,000
Thrust (Kg f) Effective: 30,432 per chamber
Actual: 31,260 per chamber
or
Effective: 104,204
Actual: 170,040
Burn time (sec.) <330?
Launch Acceleration (g's) ~1.4-1.5 or 1.3
Thrust Chambers 4, 1, 1
Stages 2, 3
Type LRICBM
Stage 1
Height (m) ~16
Diameter (m) ~2.2
Launch Weight (kg) ~60,000-61,000
Launch Thrust (kg f) ~102,880-104,000
Burn Time (sec.) ~120-130
Fuel TM-185
(20% Gasoline + 80% Kerosene)
Oxidizer AK-27I
(27% N2O4 + 73% HNO3 +
Iodium Inhibitor)
Stage 2
Height (m) ~14
Diameter (m) ~1.32-1.35
Launch Weight (kg) ~15,200
Thrust (Kg f) Effective: ~13,160
Actual: 13,300-13,380
Burn Time (sec.) 110 max
Isp. (sec.) Effective: 226 - SL
Due to vanes steering drag loss of 4-5 sec.
Actual: 230 - SL
Vac: 264
Thrust Chambers 1
Fuel TM-185
(20% Gasoline + 80% Kerosene)
Oxidizer AK-27I
(27% N2O4 + 73% HNO3 +
Iodium Inhibitor)
Propellant Mass (kg) 12,912
Stage 3
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
Propellant Solid motor*
* May have been derived from existing Chinese designs.
<link>
http://www.fas.org/nuke/guide/dprk/missile/td-2.htmAny rocket engineers out there who can calculate from these data the likely distance the missile might have flown over a seven minute period? Please post