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Start

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Start Start 1995

AKA: 15Zh58;L-1;RT-2PM;SL-18;Topol. Status: Retired 1995. First Launch: 1995-03-28. Last Launch: 1995-03-28. Number: 1 . Payload: 645 kg (1,421 lb). Thrust: 887.44 kN (199,504 lbf). Gross mass: 60,000 kg (132,000 lb). Height: 28.90 m (94.80 ft). Diameter: 1.61 m (5.28 ft). Apogee: 300 km (180 mi).

LEO Payload: 645 kg (1,421 lb) to a 300 km orbit at 30.00 degrees. Payload: 570 kg (1,250 lb) to a 400 km orbit. Launch Price $: 10.500 million in 1999 dollars.

Stage Data - Start

• Stage 1. 1 x Start-1. Gross Mass: 26,000 kg (57,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 980.000 kN (220,310 lbf). Isp: 263 sec. Burn time: 60 sec. Isp(sl): 238 sec. Diameter: 1.61 m (5.28 ft). Span: 1.61 m (5.28 ft). Length: 8.50 m (27.80 ft). Propellants: Solid. No Engines: 1. Engine: MIHT-1. Status: In Production. Comments: All estimated.

• Stage 2. 1 x Start-2. Gross Mass: 13,000 kg (28,000 lb). Empty Mass: 1,500 kg (3,300 lb). Thrust (vac): 490.000 kN (110,150 lbf). Isp: 280 sec. Burn time: 64 sec. Isp(sl): 220 sec. Diameter: 1.55 m (5.08 ft). Span: 1.55 m (5.08 ft). Length: 6.00 m (19.60 ft). Propellants: Solid. No Engines: 1. Engine: MIHT-2. Status: In Production. Comments: All estimated except stage gross mass.

• Stage 3. 1 x Start-2. Gross Mass: 13,000 kg (28,000 lb). Empty Mass: 1,500 kg (3,300 lb). Thrust (vac): 490.000 kN (110,150 lbf). Isp: 280 sec. Burn time: 64 sec. Isp(sl): 220 sec. Diameter: 1.55 m (5.08 ft). Span: 1.55 m (5.08 ft). Length: 6.00 m (19.60 ft). Propellants: Solid. No Engines: 1. Engine: MIHT-2. Status: In Production. Comments: All estimated except stage gross mass.

• Stage 4. 1 x Start-3. Gross Mass: 6,000 kg (13,200 lb). Empty Mass: 1,000 kg (2,200 lb). Thrust (vac): 245.000 kN (55,078 lbf). Isp: 280 sec. Burn time: 56 sec. Isp(sl): 220 sec. Diameter: 1.50 m (4.90 ft). Span: 1.50 m (4.90 ft). Length: 3.00 m (9.80 ft). Propellants: Solid. No Engines: 1. Engine: MIHT-3. Status: In Production. Comments: All estimated.

• Stage 5. 1 x Start-4. Gross Mass: 1,000 kg (2,200 lb). Empty Mass: 300 kg (660 lb). Thrust (vac): 9.800 kN (2,203 lbf). Isp: 295 sec. Burn time: 207 sec. Diameter: 1.40 m (4.50 ft). Span: 1.40 m (4.50 ft). Length: 2.50 m (8.20 ft). Propellants: Solid. No Engines: 1. Engine: MIHT-4. Status: In Production. Comments: All estimated.

Photo Gallery

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Start Credit: © Mark Wade

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ICBM-Derived LVs The range of launch vehicles derived from decommissioned ballistic missiles offered for sale by Russia after the cold war. Credit: © Mark Wade

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• Gurwin 1 - . Payload: TECHSAT-1. Mass: 50 kg (110 lb). Nation: Israel. Agency: RVSN. Class: Technology. Type: Navigation technology satellite. Spacecraft: Gurwin. Decay Date: 1995-03-28 .

• Oscar 29 - . Payload: ENB UNAMSAT A. Nation: Mexico. Agency: RVSN. Program: Oscar. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Oscar. UNAMSAT was an AMSAT Microsat class amateur radio satellite built by UNAM, the Autonomous University of Mexico..

• EKA - . Payload: EKA-2. Nation: Russia. Agency: RVSN. Class: Technology. Type: Navigation technology satellite. Spacecraft: EKA. Eksperimentalniy Kosmicheskiy Apparat - dummy of test satellite..