Encyclopedia Astronautica
Delta C



delc6507.jpg
Delta C no. 29
Delta C no. 29 - COSPAR 1965-007
American orbital launch vehicle. Unaugmented Thor with Delta D and solid propellant upper stages.

Payload: 82 kg (180 lb) to a GTO in 1985 dollars. Flyaway Unit Cost $: 9.590 million.

Stage Data - Delta C

  • Stage 1. 1 x Thor DM-21. Gross Mass: 48,354 kg (106,602 lb). Empty Mass: 2,948 kg (6,499 lb). Thrust (vac): 760.643 kN (170,999 lbf). Isp: 285 sec. Burn time: 164 sec. Isp(sl): 250 sec. Diameter: 2.44 m (8.00 ft). Span: 2.44 m (8.00 ft). Length: 18.41 m (60.40 ft). Propellants: Lox/Kerosene. No Engines: 1. Engine: MB-3-1. Status: Out of Production.
  • Stage 2. 1 x Delta D. Gross Mass: 2,693 kg (5,937 lb). Empty Mass: 545 kg (1,201 lb). Thrust (vac): 33.695 kN (7,575 lbf). Isp: 278 sec. Burn time: 170 sec. Isp(sl): 0.0000 sec. Diameter: 0.84 m (2.75 ft). Span: 0.84 m (2.75 ft). Length: 5.58 m (18.30 ft). Propellants: Nitric acid/UDMH. No Engines: 1. Engine: AJ10-118D. Status: Out of Production.
  • Stage 3. 1 x Altair 1. Gross Mass: 238 kg (524 lb). Empty Mass: 30 kg (66 lb). Thrust (vac): 12.450 kN (2,799 lbf). Isp: 256 sec. Burn time: 38 sec. Isp(sl): 233 sec. Diameter: 0.46 m (1.50 ft). Span: 0.46 m (1.50 ft). Length: 1.83 m (6.00 ft). Propellants: Solid. No Engines: 1. Engine: X-248. Status: Out of Production.

Status: Out of production.
Gross mass: 51,285 kg (113,064 lb).
Payload: 82 kg (180 lb).
Height: 31.00 m (101.00 ft).
Diameter: 2.44 m (8.00 ft).
Thrust: 667.20 kN (149,993 lbf).

More... - Chronology...


Associated Countries
Associated Spacecraft
  • TIROS American earth weather satellite. 12 launches, 1960.04.01 (Tiros 1) to 1966.02.28 (ESSA 2). TIROS spacecraft were the beginning of a long series of polar-orbiting meteorological satellites. More...
  • EPE American solar satellite. 4 launches, 1961.08.16 (Explorer 12) to 1964.12.21 (Explorer 26). Radiation and solar wind data. More...
  • OSO American solar satellite. 9 launches, 1962.03.07 (OSO 1) to 1975.06.21 (OSO 8). The Orbiting Solar Observatories, developed for NASA's Goddard Space Flight Center, were designed primarily as stabilized platforms for solar-oriented scientific instruments. More...
  • AE American earth atmosphere satellite. 5 launches, 1963.04.03 (Explorer 17) to 1975.11.20 (Explorer 55). Atmospheric research. More...
  • IMP American earth magnetosphere satellite. 10 launches, 1963.11.27 (Explorer 18) to 1973.10.26 (Explorer 50). More...

Associated Engines
  • AJ10-118D Aerojet Nitric acid/UDMH rocket engine. 33.7 kN. Isp=278s. Used on Delta B, Delta C, Delta D upper stages. First flight 1962. More...
  • MB-3-1 Rocketdyne Lox/Kerosene rocket engine. 760.6 kN. Out of production. Designed for booster applications. Gas generator, pump-fed. Isp=285s. Boosted Delta A, B, C, Thor Able-Star. First flight 1960. More...
  • X-248 Thiokol solid rocket engine. 12.4 kN. Isp=256s. Used on Atlas Able, Blue Scout 2, Caleb, Delta, Delta A, Delta B, Delta C. First flight 1959. More...

See also
  • Delta The Delta launch vehicle was America's longest-lived, most reliable, and lowest-cost space launch vehicle. Development began in 1955 and it continued in service in the 21st Century despite numerous candidate replacements. More...

Associated Manufacturers and Agencies
  • Douglas American manufacturer of rockets, spacecraft, and rocket engines. Boeing Huntington Beach, Huntington Beach, CA, USA. More...

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