Encyclopedia Astronautica
Thor DSV-2E


American orbital launch vehicle. Single stage vehicle.

Failures: 3. First Fail Date: 1962-06-20. Last Fail Date: 1962-10-16.

Status: Retired 1962.
Gross mass: 49,300 kg (108,600 lb).
Height: 19.40 m (63.60 ft).
Diameter: 2.44 m (8.00 ft).
Thrust: 668.00 kN (150,172 lbf).
Apogee: 500 km (310 mi).
First Launch: 1962.05.02.
Last Launch: 1962.11.01.
Number: 8 .

More... - Chronology...


Associated Countries
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...

Associated Launch Sites
  • Johnston Island US military base on this island in the Pacific Ocean. Used for rocket-launched nuclear tests in the 1950's. In the 1960's it was the site for the operational AFP-437 anti-satellite system. The system was retired in 1975. Several sounding rockets were also launched over the years, either in support of nuclear tests or in experiments related to anti-satellite technology. Known to have been used for 124 launches from 1958 to 1975, reaching up to 1158 kilometers altitude. More...

Associated Stages
  • Thor DM-19 Lox/Kerosene propellant rocket stage. Loaded/empty mass 49,340/3,125 kg. Thrust 758.71 kN. Vacuum specific impulse 282 seconds. More...

Thor DSV-2E Chronology


1962 May 2 - . 23:44 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE1. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 177.
  • TIGERFISH test - . Nation: USA. Agency: USAF. Apogee: 500 km (310 mi).

1962 June 4 - . 09:44 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE1. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 199.
  • BLUEGILL Nuclear test - . Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). Initial attempt to launch a live nuclear weapon using the Thor IRBM from Johnston Atoll. The range safety radar had been unreliable before launch,. Five minutes after launch, after shutdown of the booster, the Johnston missile tracking system failed. Unable to monitor the warhead's flight path, the range safety officer destroyed it 10 minutes later, prior to warhead detonation.

1962 June 20 - . 08:46 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE1. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 193. FAILURE: Failure. Failed Stage: 1.
  • STARFISH Nuclear test - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1962 July 9 - . 08:46 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE1. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 195.
  • STARFISH PRIME Nuclear test - . Nation: USA. Agency: USAF. Apogee: 400 km (240 mi). Successful high-altitude test of a Thor IRBM with a live nuclear warhead. The payload included test instrumentation and a W-49 warhead/Mk-4 re-entry vehicle. The 1.45 megaton bomb exploded at an altitude of 400 km. The explosion was visible 2,600 km away, at Kwajalein Atoll; an artificial aurora lasted seven minutes. The unforeseen and most militarily significant effect was the electromagnetic pulse (EMP) generated by the test. This caused power mains surges in Oahu, knocking out street lights, blowing fuses and circuit breakers, and triggering burglar alarms (and this in the days before microelectronics). The explosion supercharged the Van Allen radiation belts, resulting in several satellites malfunctioning.

1962 July 26 - . 09:13 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE1. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 180. FAILURE: Thor exploded on liftoff.. Failed Stage: 1.
  • BLUEGILL PRIME Nuclear test - . Nation: USA. Agency: USAF. Apogee: 0 km ( mi). Second attempt to launch a nuclear weapon using the Thor IRBM. The payload consisted of two re-entry vehicles, one with an instrument pod, the other with the warhead. The missile engine malfunctioned immediately on ignition. Range safety fired the destruct system whille the missile was still on the launch pad. The Johnston Island launch complex was heavily damaged and contaminated with plutonium. Three months of repairs and decontamination were necessary before tests could resume.

1962 October 16 - . 09:14 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE2. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 156. FAILURE: At 86 seconds after launch a booster failure occurred and the missile began tumbling.. Failed Stage: 1.
  • BLUEGILL DOUBLE PRIME Nuclear test - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi). The third attempt to launch a nuclear warhead using a Thor IRBM. At 86 seconds after launch a booster failure occurred and the missile began tumbling. Range safety destroyed the errant booster at 156 seconds after launch. Some radioactive fallout from the warhead was detected on Johnston Atoll.

1962 October 26 - . 09:44 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE1. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 141.
  • BLUEGILL TRIPLE PRIME Nuclear test - . Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). On the fourth attempt, a Thor IRBM was used to launch a Mk 4 Re-entry Vehicle containing a 186 kg W-50 nuclear warhead of either 200 or 400 kilotons yield. The detonation occurred at an altitude of 50 km, 31 km SSW of Johnston Atoll. A fireball formed, the colourful afterglow continuing for 30 minutes of the explosion. At this altitude the extensive disruption of the ionosphere seen in later explosions did not occur.

1962 November 1 - . 11:54 GMT - . Launch Site: Johnston Island. Launch Complex: Johnston Island LE2. LV Family: Delta. Launch Vehicle: Thor DSV-2E. LV Configuration: Thor DSV-2E 226.
  • KINGFISH Nuclear test - . Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). A Thor IRBM was used to launch a Mk 4 Reentry Vehicle containing a 186 kg W-50 nuclear warhead of either 200 or 400 kilotons yield. The detonation occurred at an altitude of 98 km, 69 km SSW of Johnston Atoll, and resulted in dramatic aurora-like effects visible as far away as Hawaii. More notably, the explosion had a massive effect on the ionosphere which disrupted radio communications over the entire central Pacific for three hours.

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