Function | Sounding rocket Test vehicle ASAT booster |
---|---|
Country of origin | United States |
Launch history | |
Launch sites | CCAFS LC-17 Johnston Atoll LE-1 & LE-2 VA LC-75 |
Total launches | 34 |
Success(es) | 28 |
Failure(s) | 6 |
The Thor DSV-2 was a series of sounding rockets, test vehicles, and anti-satellite weapons derived from the Thor Intermediate-range ballistic missile. It was also used as the first stage of several Thor-derived expendable launch systems. [1]
The DSV-2A was a two-stage rocket, consisting of a DSV-2A / MB-3-II first stage, and an Able-Star / AJ10-104D second stage. [2] It was launched eight times between 1963 and 1965 from Vandenberg. [2]
S/N | Date | Launch Site | Payload | Result |
---|---|---|---|---|
Thor 375 | 1963-09-28 | VA LC-75 | Transit 5BN-1 / Transit 5E-1 | Success |
Thor 385 | 1963-12-05 | VA LC-75 | Transit 5BN-2 / Transit 5E-3 | Success |
Thor 379 | 1964-04-21 | VA LC-75 | Transit 5BN-3 / Transit 5E-2 | Failure |
Thor 423 | 1964-10-06 | VA LC-75 | Transit-O 1/ Dragsphere 1 / Dragsphere 2 | |
Thor 427 | 1964-12-13 | VA LC-75 | Transit-O 2 / Transit 5E-5 | |
Thor 440 | 1965-03-11 | VA LC-75 | Transit-O 3 / SECOR 2 | Partial success |
Thor 447 | 1965-06-24 | VA LC-75 | Transit-O 4 | |
Thor 455 | 1965-08-13 | VA LC-75 | Transit-O 5 / Dodecapole 2 / Long Rod / Tempsat 1 / Surcal 5 / Calsphere 2 |
The DSV-2D was launched twice in 1962, [3] conducting suborbital research flights for the development of the Program 437 ASAT. It was a single-stage vehicle, consisting of a Thor DM-21. Launches were conducted from Cape Canaveral Air Force Station Launch Complex 17A.
S/N | Date | Launch Site | Payload | Orbit |
---|---|---|---|---|
Thor 337 | 1962-01-15 | CCAFS LC-17A | Big Shot 1 (AVT 1) | Suborbital |
Thor 338 | 1962-07-18 | CCAFS LC-17A | Big Shot 2 (AVT 2) | Suborbital |
The DSV-2E was a single-stage vehicle, using a Thor DM-19. It was launched eight times in 1962, including several nuclear weapons tests as part of Operation Fishbowl. [4] Four launches failed, all of which were carrying live nuclear warheads. [4] Launches were conducted from Launch Emplacements 1 and 2 on Johnston Atoll.
S/N | Date | Launch Site | Payload | Orbit | Result |
---|---|---|---|---|---|
Thor 177 | 1962-05-02 | Johnston LE-1 | Tigerfish (R/D) | Suborbital | Success |
Thor 199 | 1962-06-04 | Johnston LE-1 | Bluegill | Suborbital | Radar contact lost 5 minutes after launch. RSO destruct command sent. |
Thor 193 | 1962-06-20 | Johnston LE-1 | Starfish | Suborbital | RVs caused turbine exhaust gas to enter the thrust section, overheating and weakening the engine mounts. Engine broke loose and ruptured the propellant tanks T+59 seconds. Warhead destroyed by RSO T+65 seconds. |
Thor 195 | 1962-07-09 | Johnston LE-1 | Starfish Prime | Suborbital | Success |
Thor 180 | 1962-07-26 | Johnston LE-1 | Bluegill Prime | Suborbital | Stuck LOX valve caused loss of thrust and fire on the launch stand. Range Safety Officer destroyed the missile and warhead. Launch area extensively contaminated with plutonium. |
Thor 156 | 1962-10-16 | Johnston LE-2 | Bluegill Double Prime | Suborbital | Flight control failure T+85 seconds. RSO T+156 seconds. |
Thor 141 | 1962-10-26 | Johnston LE-1 | Bluegill Triple Prime | Suborbital | Success |
Thor 226 | 1962-11-01 | Johnston LE-2 | Kingfish | Suborbital | Success |
The DSV-2F was a single-stage vehicle consisting of a Thor DM-19, like the DSV-2E. Three were launched between 1963 and 1964, as part of Project ASSET, [5] which involved launching a sub-scale mockup of the X-20 Dyna-Soar to test materials for the larger spacecraft. Launches were conducted from Cape Canaveral Air Force Station Launch Complex 17B.
S/N | Date | Launch Site | Payload | Orbit | Result |
---|---|---|---|---|---|
Thor 232 | 1963-09-18 | CCAFS LC-17B | ASSET-1 (ASSET ASV 1) | Suborbital | Success |
Thor 260 | 1964-10-28 | CCAFS LC-17B | ASSET-4 (ASSET-AEV 1) | Suborbital | Success |
Thor 247 | 1964-12-09 | CCAFS LC-17B | ASSET-5 (ASSET-AEV 2) | Suborbital | Success |
The DSV-2G was a two-stage rocket, consisting of a Thor DM-19 first stage, and a Delta second stage. Three were launched between 1964 and 1965 as part of Project ASSET. [6] Launches were conducted from Cape Canaveral Air Force Station Launch Complex 17B.
S/N | Date | Launch Site | Payload | Orbit | Result |
---|---|---|---|---|---|
Thor 240 | 1964-03-24 | CCAFS LC-17B | ASSET-2 (ASSET-ASV 2) | Suborbital | Atmospheric flight, second stage fired intermittently, destroyed by range safety |
Thor 250 | 1964-07-22 | CCAFS LC-17B | ASSET-3 (ASSET-ASV 3) | Suborbital | Success |
Thor 248 | 1965-02-23 | CCAFS LC-17B | ASSET-6 (ASSET-ASV 4) | Suborbital | Success |
The DSV-2J was an operational nuclear anti-satellite weapon. 18 were launched between 1964 and 1975. [7] Most flights were non-intercept tests of the rocket's anti-satellite capabilities, however some later launches carried research payloads. Launches were conducted from Launch Emplacements 1 and 2 on Johnston Atoll.
S/N | Date | Launch Site | Payload | Result |
---|---|---|---|---|
Thor 299 | 14.02.1964 | Johnston LE-1 | AFP-437 (#1) | Success |
Thor 209 | 02.03.1964 | Johnston LE-1 | AFP-437 (#2) | Success |
Thor 290 | 21.04.1964 | Johnston LE-2 | AFP-437 (#3) | Success |
Thor 227 | 28.05.1964 | Johnston LE-2 | AFP-437 (#4) | Failure |
Thor 236 | 16.11.1964 | Johnston LE-1 | AFP-437 (#5) | Success |
Thor 155 | 05.04.1965 | Johnston LE-2 | AFP-437 (#6) | Success |
Thor 188 | 07.12.1965 | Johnston LE-2 | AFP-437AP (#1) | Success |
Thor 242 | 18.01.1966 | Johnston LE-2 | AFP-437AP (#2) | Success |
Thor 196 | 12.03.1966 | Johnston LE-2 | AFP-437AP (#3) | Success |
Thor 289 | 02.07.1966 | Johnston LE-2 | AFP-437AP (#4) | Success |
Thor 168 | 31.03.1967 | Johnston LE-1 | AFP-437 (#7) | Success |
Thor 205 | 14.05.1968 | Johnston LE-1 | AFP-437 (#8) | Success |
Thor 252 | 20.11.1968 | Johnston LE-1 | AFP-437 (#9) | Success |
Thor 152 | 27.03.1970 | Johnston LE-1 | AFP-437 (#10) | Success |
Thor 225 | 24.04.1970 | Johnston LE-2 | SDP | Partial Success |
Thor 271 | 24.09.1970 | Johnston LE-2 | HAP/SXRE | Success |
Thor 201 | 19.09.1975 | Johnston LE-2 | BMDTTP 1 (DG-5) | Success |
Thor 274 | 06.11.1975 | Johnston LE-2 | BMDTTP 2 (DG-3) | Success |
The PGM-17A Thor was the first operative ballistic missile of the United States Air Force (USAF). It was named after the Norse god of thunder. It was deployed in the United Kingdom between 1959 and September 1963 as an intermediate-range ballistic missile (IRBM) with thermonuclear warheads. Thor was 65 feet (20 m) in height and 8 feet (2.4 m) in diameter.
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.
Program 437 was the second anti-satellite weapons program of the U.S. military. The US anti-satellite weapons program began development in the early 1960s and was officially discontinued on 1 April 1975. Program 437 was approved for development by U.S. Secretary of Defense Robert McNamara on November 20, 1962, after a series of tests involving high altitude nuclear explosions. The program's facilities were located on Johnston Island, an isolated island in the north central Pacific Ocean.
Space Launch Complex 17 (SLC-17), previously designated Launch Complex 17 (LC-17), was a launch site at Cape Canaveral Air Force Station (CCAFS), Florida used for Thor and Delta launch vehicles launches between 1958 and 2011.
The Delta G, or Thor-Delta G was an American expendable launch system used to launch two biological research satellites in 1966 and 1967. It was a member of the Delta family of rockets.
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-Ablestar, or Thor-Able-Star, also known as Thor-Epsilon was an early American expendable launch system consisting of a PGM-17 Thor missile, with an Ablestar upper stage. It was a member of the Thor family of rockets, and was derived from the Thor-Able.
The Thor DSV-2U or Thor LV-2F Star-37XE Star-37S-ISS was an American expendable launch system used to launch five DMSP weather satellites between 1976 and 1980. It was a member of the Thor family of rockets, and a derivative of the Thor DSV-2.
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 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 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 L, Thor-Delta L, or Thrust-Augmented Long Tank Thor-Delta was a US expendable launch system used to launch the Pioneer E and TETR satellites in 1969 (failed) and HEOS satellite in 1972. 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.
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The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.
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.