Tips :

1) ignite the nuclear engine when AGL is higer then 10000 M

2) don't pitch before and after booster seperation for a 10 seconds, because rocket can start spinning around


Soviet Union nuclear-powered orbital launch vehicle. First large space launcher considered in the Soviet Union. It would have had the same layout as the R-7, but with six strap-ons increased in size by 50%. The core, igniting at altitude, used a nuclear thermal engine using ammonia as propellant. Dropped in favor of development of conventional chemical propulsion.
Status: Cancelled 1959. Payload: 40,000 kg (88,000 lb). Thrust: 12,422.80 kN (2,792,757 lbf). Gross mass: 888,000 kg (1,957,000 lb). Height: 44.00 m (144.00 ft). Diameter: 3.33 m (10.92 ft). Apogee: 185 km (114 mi).

LEO Payload: 40,000 kg (88,000 lb) to a 185 km orbit.


Stage Data - YaKhR-2

Stage 0. 6 x YaKhR-2 Strap-on. Gross Mass: 110,000 kg (240,000 lb). Empty Mass: 8,250 kg (18,180 lb). Thrust (vac): 2,393.724 kN (538,131 lbf). Isp: 311 sec. Burn time: 125 sec. Isp(sl): 269 sec. Diameter: 3.33 m (10.92 ft). Span: 3.33 m (10.92 ft). Length: 27.00 m (88.00 ft). Propellants: Lox/Kerosene. No Engines: 6. Engine: RD-111. Status: Study 1959. Comments: R-7 strap-ons increased in size dimensionally 50%, equipped with 6 engines from R-9. Boost nuclear thermal core stage to altitude before ignition of nuclear engine. Masses calculated based on vehicle total weight and performance.
Stage 1. 1 x YaKhR-2 Core. Gross Mass: 180,000 kg (390,000 lb). Empty Mass: 22,000 kg (48,000 lb). Thrust (vac): 1,660.000 kN (373,180 lbf). Isp: 470 sec. Burn time: 430 sec. Isp(sl): 430 sec. Diameter: 3.33 m (10.92 ft). Span: 3.33 m (10.92 ft). Length: 37.00 m (121.00 ft). Propellants: Nuclear/Ammonia. No Engines: 1. Engine: YaRD OKB-456. Status: Study 1959. Comments: Engines in development by Bondaryuk and Glushko. Alternate propellants ammonia only or ammonia/alcohol mixture. Four expansion nozzles fed by single reactor. Masses calculated based on given vehicle gross weight and performance.

From : astronautix

GENERAL INFO

  • Created On: Android
  • Game Version: 0.9.802.0
  • Price: $63,748k
  • Number of Parts: 301
  • Dimensions: 50 m x 15 m x 13 m

PERFORMANCE

  • Total Delta V: 2.4km/s
  • Total Thrust: 25.4MN
  • Engines: 52
  • Wet Mass: 4.21E+5kg
  • Dry Mass: 1.72E+5kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 36 1.8km/s 9.1MN 58s 4.21E+5kg
2 4 612m/s 844kN 4.9m 4.21E+5kg
3 0 0m/s 0N 0s 63,532kg

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