| Taepodong 1-2 |
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Model: Taepodong 1-2. Gross Mass: 7,505 kg (16,545 lb). Empty Mass: 1,456 kg (3,209 lb). Thrust (vac): 144.334 kN (32,448 lbf). Isp: 255 sec. Burn time: 176 sec. Propellants: Nitric acid/UDMH. Isp(sl): 232 sec. Diameter: 0.96 m (3.14 ft). Span: 1.10 m (3.60 ft). Length: 12.00 m (39.00 ft). Country: Korea North. No Engines: 1. Motor: Nodong. Status: Retired 1998. First Flight: 1998. Last Flight: 1998. No Launched: 1. Included 100 kg spin table for spin-up of third stage prior to release. Burn time is 33.7 seconds at full thrust, 142.3 seconds at half thrust. Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |