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DOT
Part of Sergeant
American sounding rocket. Three stage vehicle consisting of 2 x Recruit + 1 x Castor + 1 x Star 26C

Status: Retired 1981. First Launch: 1980-02-05. Last Launch: 1981-06-12. Number: 3 . Thrust: 586.00 kN (131,738 lbf). Gross mass: 5,500 kg (12,100 lb). Height: 11.60 m (38.00 ft). Diameter: 0.79 m (2.59 ft). Apogee: 300 km (180 mi).

Subtopics
DOK-10 Isayev monopropellant rocket engine. In Production. Pressure-fed monopropellant engine. Thermal decomposition of hydrazine by an iridium-based catalyst, which heated to increase stability. 40,000 ignitions
DOK-50 Isayev monopropellant rocket engine. In Production. Pressure-fed monopropellant engine. Thermal decomposition of hydrazine by an iridium-based catalyst, which heated to increase stability. 40,000 ignitions
DOT-25 Isayev monopropellant rocket engine. In Production. Pressure-fed monopropellant engine. Thermal decomposition of hydrazine by a wire catalyst, which is electrically heated to 620 K. 60,000 ignitions
DOT-5 Isayev monopropellant rocket engine. In Production. Pressure-fed monopropellant engine. Thermal decomposition of hydrazine by a wire catalyst, which is electrically heated to 620 K. 550,000 ignitions
Country: USA. Launch Sites: Kwajalein, Kwajalein RN. Stages: 1.5KS35000, Castor 1, Star 26C. Bibliography: 2.
1980 February 5 - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Sergeant. Launch Vehicle: DOT.
1980 September 17 - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Sergeant. Launch Vehicle: DOT.
1981 June 12 - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Sergeant. Launch Vehicle: DOT.
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