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Launch Complex: LE1.
Johnston Island. Latitude: 16.7288 deg. Longitude: -169.5398 deg. Used by: Delta. First Launch: 1962-05-02. Last Launch: 1970-03-27. Number Launches: 13. Launch Emplacement 1

LE1 Chronology

1962 May 2 - 23:44 GMT - Launch Vehicle: Delta. Thor DSV-2E 177 TIGERFISH test Agency: USAF. Apogee: 500 km (310 mi).

1962 June 4 - 09:44 GMT - Launch Vehicle: Delta. Thor DSV-2E 199 BLUEGILL Nuclear test 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 Vehicle: Delta. Thor DSV-2E 193 FAILURE: Failure. STARFISH Nuclear test Agency: USAF. Apogee: 10 km (6 mi).

1962 July 9 - 08:46 GMT - Launch Vehicle: Delta. Thor DSV-2E 195 STARFISH PRIME Nuclear test 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 Vehicle: Delta. Thor DSV-2E 180 FAILURE: Thor exploded on liftoff. BLUEGILL PRIME Nuclear test 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 26 - 09:44 GMT - Launch Vehicle: Delta. Thor DSV-2E 141 BLUEGILL TRIPLE PRIME Nuclear test 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.

1964 February 14 - 07:47 GMT - Launch Vehicle: Delta. Thor DSV-2J 299 (20002) AFP-437 demonstration interceptor mission Agency: USAF/DACO. Apogee: 1,000 km (600 mi).

1964 March 1 - 06:40 GMT - Launch Vehicle: Delta. Thor DSV-2J 209 (20006) AFP-437 demonstration interceptor mission Agency: USAF 10ADS. Apogee: 674 km (418 mi).

1964 November 16 - 06:57 GMT - Launch Vehicle: Delta. Thor DSV-2J 236 AFP-437 combat training interceptor mission Agency: USAF. Apogee: 1,148 km (713 mi).

1967 March 31 - 06:44 GMT - Launch Vehicle: Delta. Thor DSV-2J 168 AFP-437 combat evaluation interceptor mission Agency: USAF. Apogee: 484 km (300 mi).

1968 May 14 - 07:05 GMT - Launch Vehicle: Delta. Thor DSV-2J 205 AFP-437 combat evaluation interceptor mission Agency: USAF. Apogee: 823 km (511 mi).

1968 November 20 - 07:08 GMT - Launch Vehicle: Delta. Thor DSV-2J 252 AFP-437 combat evaluation interceptor mission Agency: USAF. Apogee: 1,158 km (719 mi).

1970 March 27 - 07:37 GMT - Launch Vehicle: Delta. Thor DSV-2J 152 AFP-437 Interceptor mission Agency: USAF. Apogee: 1,074 km (667 mi).


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© Mark Wade, 1997 - 2008 except where otherwise noted.