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Soltan
Part of Titan
American orbital launch vehicle. The progenitor of the Titan 3 was this design, which used two, 3 segment, 100 inch diameter solid rocket boosters. The 100 inch segmented boosters had already been ground-fired by Aerojet. However the final decision was to develop the more-capable Titan 3C with 5 segment, 120 inch diameter solid rocket boosters.

Status: Study 1961. Payload: 8,030 kg (17,700 lb). Thrust: 6,021.00 kN (1,353,574 lbf). Gross mass: 388,560 kg (856,620 lb). Height: 40.40 m (132.50 ft). Diameter: 3.05 m (10.00 ft). Span: 15.70 m (51.50 ft). Apogee: 148 km (91 mi).

The original design submitted for the SLV-4 competition had two 2.54 m diameter solid boosters.

LEO Payload: 8,030 kg (17,700 lb) to a 148 km orbit at 28.00 degrees.

Stage Data - Soltan



Family: orbital launch vehicle. Country: USA. Spacecraft: Dynasoar. Stages: Titan 2-1, Titan 2-2, 100 inch solid. Agency: Martin.

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