Function | Expendable launch system |
---|---|
Manufacturer | Douglas Aircraft Company |
Country of origin | United States |
Launch history | |
Status | Retired |
Launch sites | Cape Canaveral LC-17 |
Total launches | 13 |
Success(es) | 12 |
Failure(s) | 1 |
First flight | 27 November 1963 |
Last flight | 22 January 1969 |
The Delta C, or Thor-Delta C was an American expendable launch system used for thirteen orbital launches between 1963 and 1969. It was a member of the Delta family of rockets.
The first stage was a Thor missile in the DSV-2A (MB-3-II) configuration, and the second stage was the Delta D (AJ-10-118D), which was derived from the earlier Delta. [1] The baseline Delta C used an Altair-2 (X-258) third stage, [1] whilst the Delta C1 had an FW-4D third stage, which provided a higher payload capacity than the Altair. It is unclear whether two or three launches were made using the C1 configuration.
The Delta C was launched from Cape Canaveral Air Force Station Launch Complex 17. Most launches carried NASA research satellites into low Earth orbit. [2] [1]
Variant | S/N | Date | Launch Site | Payload | Result |
---|---|---|---|---|---|
Delta C | 387/D-21 | 27.11.1963 | CC LC-17B | Explorer 18 (IMP A) | Success |
Delta C | 392/D-26 | 04.10.1964 | CC LC-17A | Explorer 21 (IMP B) | Success |
Delta C | 393/D-27 | 21.12.1964 | CC LC-17A | Explorer 26 (EPE D) | Success |
Delta C | 374/D-28 | 22.01.1965 | CC LC-17A | TIROS 9 | Success |
Delta C | 411/D-29 | 03.02.1965 | CC LC-17B | OSO 2 | Success |
Delta C | 441/D-31 | 29.05.1965 | CC LC-17B | Explorer 28 (IMP C) | Success |
Delta C | 415/D-32 | 02.07.1965 | CC LC-17B | TIROS 10 | Success |
Delta C | 434/D-33 | 25.08.1965 | CC LC-17B | OSO C | Failure |
Delta C | 445/D-36 | 03.02.1966 | CC LC-17A | ESSA 1 | Success |
Delta C | 431/D-46 | 08.03.1967 | CC LC-17A | OSO 3 | Success |
Delta C | 490/D-53 | 18.10.1967 | CC LC-17B | OSO 4 | Success |
Delta C1 | 436/D-38 | 25.05.1966 | CC LC-17B | Explorer 32 (AE B) | Success |
Delta C1 | 487/D-64 | 22.01.1969 | CC LC-17B | OSO 5 | Success |
The Delta rocket family was a versatile range of American rocket-powered expendable launch systems that provided space launch capability in the United States from 1960 to 2024. Japan also launched license-built derivatives from 1975 to 1992. More than 300 Delta rockets were launched with a 95% success rate. The series was phased out in favor of the Vulcan Centaur, with the Delta IV Heavy rocket's last launch occurring on April 9, 2024.
The Thor-Able was an American expendable launch system and sounding rocket used for a series of re-entry vehicle tests and satellite launches between 1958 and 1960.
The Scout family of rockets were American launch vehicles designed to place small satellites into orbit around the Earth. The Scout multistage rocket was the first orbital launch vehicle to be entirely composed of solid fuel stages. It was also the only vehicle of that type until the successful launch of the Japanese Lambda 4S in 1970.
The Thor-Burner was an American expendable launch system, a member of the Thor rocket family. It consisted of a Thor missile, with one or two Burner upper stages. It was used between 1965 and 1976 to orbit a number of satellites, most commonly Defense Meteorological Satellite Program (DMSP) weather satellites. Twenty-four were launched, of which two failed. It weighed 51,810 kg and was 24 metres tall.
The Altair was a solid-fuel rocket with a fiberglass casing, initially developed for use as the third stage of Vanguard rockets in 1959. It was manufactured by Allegany Ballistics Laboratory (ABL) as the X-248. It was also sometimes called the Burner 1.
The Delta E, or Thor-Delta E was an American expendable launch system used for twenty-three orbital launches between 1965 and 1971. It was a member of the Delta family of rockets.
The Thor-Delta, also known as Delta DM-19 or just Delta was an early American expendable launch system used for 12 orbital launches in the early 1960s. A derivative of the Thor-Able, it was a member of the Thor family of rockets, and the first member of the Delta family.
The Delta A, or Thor-Delta A was an American expendable launch system used to launch two Explorer spacecraft in October 1962. A derivative of the Thor-Delta, it was a member of the Delta family of launch vehicles. The Thor-Delta itself was a Thor booster with an Able second stage and Altair third stage.
The Delta B, or Thor-Delta B was an American expendable launch system used for nine orbital launches between 1962 and 1964. A derivative of the Thor-Delta, it was a member of the Delta family of rockets.
The Delta D, Thrust Augmented Delta or Thor-Delta D was an American expendable launch system used to launch two communications satellites in 1964 and 1965. It was derived from the Delta C, and was a member of the Delta family of rockets.
The Delta J or Thor-Delta J was an American expendable launch system of the late 1960s. Only one was launched, with the Explorer 38 spacecraft. It was a member of the Delta family of rockets.
The Delta M or Thor-Delta M was an American expendable launch system used for thirteen orbital launches between 1968 and 1971. It was a member of the Delta family of rockets.
The Delta N or Thor-Delta N was an American expendable launch system used for nine orbital launches between 1968 and 1972. It was a member of the Delta family of rockets, and the last Delta to be given an alphabetical designation - subsequent rockets were designated using a four digit numerical code.
The Delta 0100 series, also Delta 100, 0300 or 300 series, was an American expendable launch system which conducted orbital launches between 1968 and 1972. It was a member of the Delta family of rockets, and the first to be designated using a four digit numerical code. Two variants were flown, individually designated Delta 0300 and Delta 0900.
The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets, sometimes called Thorad Delta. Several variants existed, which were differentiated by a four digit numerical code. The Delta 1000, 2000 and 3000 series used surplus NASA Apollo program rockets engines for its first and second stages.
The Delta 4000 series was an American expendable launch system which was used to conduct two orbital launches in 1989 and 1990. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 4925 was launched. The designations used a four digit numerical code to store information on the configuration of the rocket. It was built from a combination of spare parts left over from earlier Delta rockets, which were being retired, and parts from the Delta II 6000-series, which was just entering service.
The Delta 5000 series was an American expendable launch system which was used to conduct an orbital launch in 1989. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 5920 was launched. The designation used a four digit numerical code to store information on the configuration of the rocket. It was built from a combination of spare parts left over from earlier Delta rockets, which were being retired, and parts from the Delta II 6000-series, which was just entering service.