1959 December 12 - 17:11 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I C-3 FAILURE: Exploded just above pad. RVX-3 Re-entry Vehicle test Agency: USAF. Apogee: 0 km ( mi). First Titan ICBM launching testing second stage was unsuccessful at AMR.

1960 February 5 - 21:46 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I C-4 FAILURE: Failure. RVX-3 Re-entry Vehicle test Agency: USAF. Apogee: 0 km ( mi).

1960 March 8 - 18:00 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I C-1 FAILURE: Failure. RVX-3 Re-entry Vehicle test Agency: USAF. Apogee: 0 km ( mi).

1960 April 8 - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I C-5 RVX-3 Re-entry Vehicle test Agency: USAF. Apogee: 1,000 km (600 mi).

1960 April 28 - 20:18 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I C-6 RVX-3 Re-entry Vehicle test Agency: USAF. Apogee: 1,000 km (600 mi).

1960 May 27 - 17:20 GMT - Launch Vehicle: Titan. LV Model: Titan 1 . Titan I G-9 RVX-4 test Agency: USAF. Apogee: 1,000 km (600 mi).

1962 March 16 - 18:09 GMT - Launch Vehicle: Titan. LV Model: Titan 2 . Titan II N-2 Mk 6 re-entry vehicle test launch Agency: USAF. Apogee: 1,300 km (800 mi). The Air Force successfully launched a Titan II intercontinental ballistic missile. This was the first full-scale test of the vehicle; it flew 8000 km out over the Atlantic Ocean.

1962 July 25 - 16:17 GMT - Launch Vehicle: Titan. LV Model: Titan 2 . Titan II N-4 Mk 6 re-entry vehicle test launch Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 October 12 - 16:24 GMT - Launch Vehicle: Titan. LV Model: Titan 2 . Titan II N-9 Mk 6 re-entry vehicle test launch Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 December 6 - 20:31 GMT - Launch Vehicle: Titan. LV Model: Titan 2 . Titan II N-11 FAILURE: Failure. Mk 4 re-entry vehicle test Agency: USAF AFSC. Apogee: 500 km (310 mi). Titan II flight N-11, the eighth in a series being conducted by the Air Force to develop the weapon system, was launched from Cape Canaveral. It carried a design change intended to reduce the amplitude of longitudinal oscillations which had appeared during first stage operation on all seven previous Titan II flights. This phenomenon, which subsequently became known as POGO, generated g-forces as high as nine in the first stage and over three at the position on the missile corresponding to the location of the spacecraft on the Gemini launch vehicle. Fearing the potentially adverse effect on astronaut performance of such superimposed g-forces, NASA established 0.25g at 11 cycles per second as the maximum level tolerable for Gemini flights. As a first try at solving the POGO problem, Titan II N-11 carried standpipes in each leg of the stage I oxidizer feed lines to interrupt the coupling between the missile's structure and its propulsion system. This coupling was presumed to be the cause of the instability. Postflight analysis, however, revealed that the POGO fix was unsuccessful; longitudinal oscillation had actually been multiplied by a factor of two.

1963 January 10 - Launch Vehicle: Titan. LV Model: Titan 2 . Titan II N-15 FAILURE: Failure. Mk 6 re-entry vehicle test launch Agency: USAF AFSC. Apogee: 500 km (310 mi).

1963 May 9 - Launch Vehicle: Titan. LV Model: Titan 2 . Titan II N-14 FAILURE: Failure. Research and development test Agency: USAF AFSC. Apogee: 1,000 km (600 mi). Mk 6 re-entry vehicle.

1963 May 29 - 16:56 GMT - Launch Vehicle: Titan. LV Model: Titan 2 . Titan II N-20 FAILURE: Failed 55 seconds after launch. Research and development test Agency: USAF AFSC. Titan II flight N-20, the 19th in the series of Air Force research and development flights, was launched from Cape Canaveral. It carried oxidizer standpipes and fuel accumulators to suppress longitudinal oscillations (POGO). During the spring of 1963, static firings of this configuration had been successful enough to confirm the hypothesis that POGO was caused by coupling between the missile structure and its propulsion system, resulting in an unstable closed loop system. Standpipes and accumulators, by interrupting the coupling reduced the source of instability. Flight N-20 failed 55 seconds after launch and yielded no POGO data. Although the failure was not attributed to the installed POGO fix, Air Force Ballistics Systems Division decided officially that no further Titan II development flights would carry the POGO fix because so few test flights remained to qualify the weapon system operationally. This decision did not stand, however, and the POGO fix was flown again on N-25 (November 1), as well as on two later flights.

1974 May 7 - 19:00 GMT - Launch Vehicle: Pershing. Pershing 1A 103 P-280 US 7th Army 81st Field Artillery/1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1974 May 7 - 19:15 GMT - Launch Vehicle: Pershing. Pershing 1A 104 P-281 US 7th Army 81st Field Artillery/1st Battalion Battery C/D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1974 May 7 - 20:05 GMT - Launch Vehicle: Pershing. Pershing 1A 102 P-282 US 7th Army 81st Field Artillery/1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1974 May 7 - 20:21 GMT - Launch Vehicle: Pershing. Pershing 1A 101 P-283 US 7th Army 81st Field Artillery/1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1974 May 21 - Launch Vehicle: Pershing. Pershing 1A 109 FAILURE: Failure. P-284 US 7th Army Operational test Agency: USA. Apogee: 250 km (150 mi).

1974 May 21 - 13:04 GMT - Launch Vehicle: Pershing. Pershing 1A 110 P-285 US 7th Army Operational test Agency: USA. Apogee: 250 km (150 mi).

1974 May 21 - 13:18 GMT - Launch Vehicle: Pershing. Pershing 1A 111 P-286 US 7th Army Operational test Agency: USA. Apogee: 250 km (150 mi).

1974 May 21 - 14:28 GMT - Launch Vehicle: Pershing. Pershing 1A 112 P-287 US 7th Army Operational test Agency: USA. Apogee: 250 km (150 mi).

1974 May 31 - 19:00 GMT - Launch Vehicle: Pershing. Pershing 1A 105 FAILURE: Failure. P-288 Operational test Agency: USA. Apogee: 0 km ( mi).

1974 May 31 - 19:15 GMT - Launch Vehicle: Pershing. Pershing 1A 106 P-289 Operational test Agency: USA. Apogee: 250 km (150 mi).

1974 May 31 - 20:05 GMT - Launch Vehicle: Pershing. Pershing 1A 107 P-290 Operational test Agency: USA. Apogee: 250 km (150 mi).

1974 May 31 - 20:21 GMT - Launch Vehicle: Pershing. Pershing 1A 108 P-291 Operational test Agency: USA. Apogee: 250 km (150 mi).

1975 July 23 - 15:04 GMT - Launch Vehicle: Pershing. Pershing 1A 37 P-308 US 7th Army 84th Field Artillery/3rd Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 July 23 - 16:38 GMT - Launch Vehicle: Pershing. Pershing 1A 38 P-309 US 7th Army 84th Field Artillery/3rd Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 July 23 - 16:53 GMT - Launch Vehicle: Pershing. Pershing 1A 39 P-310 S 7th Army 84th Field Artillery/3rd Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 July 24 - 18:49 GMT - Launch Vehicle: Pershing. Pershing 1A 40 P-311 US 7th Army 84th Field Artillery/3rd Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 August 5 - 16:04 GMT - Launch Vehicle: Pershing. Pershing 1A 41 P-312 US 7th Army 81st Field Artillery/1st Battalion Battery C/D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 August 5 - 16:20 GMT - Launch Vehicle: Pershing. Pershing 1A 42 FAILURE: Failure. P-313 US 7th Army 81st Field Artillery/1st Battalion Battery C/D operational test launch Agency: USA. Apogee: 0 km ( mi).

1975 August 5 - 18:16 GMT - Launch Vehicle: Pershing. Pershing 1A 43 P-314 US 7th Army 81st Field Artillery/1st Battalion Battery C/D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 August 5 - 18:32 GMT - Launch Vehicle: Pershing. Pershing 1A 44 P-315 US 7th Army 81st Field Artillery/1st Battalion Battery C/D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 August 25 - 15:54 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-45 FAILURE: Failure. P-316 US 7th Army 41st Field Artillery /1st Battalion Battery C operational test launch Agency: USA. Apogee: 0 km ( mi).

1975 August 25 - 17:32 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-46 P-317 US 7th Army 41st Field Artillery /1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 August 26 - 18:32 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-47 P-318 US 7th Army 41st Field Artillery /1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1975 August 26 - 18:49 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-48 FAILURE: Failure. P-319 US 7th Army 41st Field Artillery /1st Battalion Battery C operational test launch Agency: USA. Apogee: 0 km ( mi).

1976 October 26 - 18:06 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-49 US 7th Army 84th Field Artillery/3rd Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1976 October 26 - 19:12 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-50 US 7th Army 84th Field Artillery/3rd Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1976 October 26 - 20:21 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-51 US 7th Army 84th Field Artillery/3rd Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1976 October 26 - 20:39 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-52 US 7th Army 84th Field Artillery/3rd Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1977 February 17 - 18:12 GMT - Launch Vehicle: Pershing. US 7th Army 84th Field Artillery/3rd Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1977 March 2 - 18:28 GMT - Launch Vehicle: Pershing. US 7th Army 41st Field Artillery/1st Batallion Battalion B operational test launch Agency: USA. Apogee: 250 km (150 mi).

1977 March 2 - 18:53 GMT - Launch Vehicle: Pershing. FAILURE: Failure. US 7th Army 41st Field Artillery/1st Battalion Battery B operational test launch Agency: USA. Apogee: 0 km ( mi).

1977 March 2 - 20:31 GMT - Launch Vehicle: Pershing. US 7th Army 41st Field Artillery/1st Battalion Battery Boperational test launch Agency: USA. Apogee: 250 km (150 mi).

1977 March 2 - 21:42 GMT - Launch Vehicle: Pershing. FAILURE: Failure. US 7th Army 41st Field Artillery/1st Battalion Battery B operational test launch Agency: USA. Apogee: 0 km ( mi).

1978 July 13 - 14:37 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-111 US 7th Army 81st Field Artillery/1st Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 July 13 - 16:57 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-112 US 7th Army 81st Field Artillery/1st Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 July 13 - 18:09 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-113 US 7th Army 81st Field Artillery/1st Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 July 25 - 14:30 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-115 US 7th Army 84th Field Artillery/3rd Battalion Battery D operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 July 25 - 14:48 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-114 US 7th Army 84th Field Artillery/3rd Battalion Battery A operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 July 25 - 15:06 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-116 US 7th Army 84th Field Artillery/3rd Battalion Battery A operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 August 25 - 13:06 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-117 US 7th Army 41st Field Artillery /1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 August 25 - 13:23 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-118 US 7th Army 41st Field Artillery /1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1978 August 25 - 13:53 GMT - Launch Vehicle: Pershing. Pershing 1A FOT-119 US 7th Army 41st Field Artillery /1st Battalion Battery C operational test launch Agency: USA. Apogee: 250 km (150 mi).

1979 February 22 - 14:43 GMT - Launch Vehicle: Pershing. FOT-121 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 February 22 - 15:00 GMT - Launch Vehicle: Pershing. FOT-122 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 February 22 - 15:19 GMT - Launch Vehicle: Pershing. FOT-120 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 April 25 - 15:03 GMT - Launch Vehicle: Pershing. FOT-125 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 April 25 - 15:17 GMT - Launch Vehicle: Pershing. FOT-124 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 April 25 - 15:40 GMT - Launch Vehicle: Pershing. FOT-123 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 May 9 - 17:00 GMT - Launch Vehicle: Pershing. FOT-128 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 May 9 - 18:29 GMT - Launch Vehicle: Pershing. FOT-126 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1979 May 9 - 18:50 GMT - Launch Vehicle: Pershing. FOT-127 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 February 12 - 15:51 GMT - Launch Vehicle: Pershing. FOT-131 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 February 12 - 16:27 GMT - Launch Vehicle: Pershing. FOT-129 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 April 23 - 15:04 GMT - Launch Vehicle: Pershing. FOT-132 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 April 23 - 15:22 GMT - Launch Vehicle: Pershing. FOT-133 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 April 23 - 15:39 GMT - Launch Vehicle: Pershing. FOT-134 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 April 23 - 16:05 GMT - Launch Vehicle: Pershing. FOT-135 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 May 7 - 14:40 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1980 May 7 - 14:59 GMT - Launch Vehicle: Pershing. FOT-136 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 May 7 - 15:58 GMT - Launch Vehicle: Pershing. FOT-137 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1980 May 15 - 14:51 GMT - Launch Vehicle: Pershing. FOT-138 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 February 4 - 15:00 GMT - Launch Vehicle: Pershing. FOT-141 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 February 4 - 15:33 GMT - Launch Vehicle: Pershing. FOT-139 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 February 4 - 15:53 GMT - Launch Vehicle: Pershing. FOT-140 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 February 17 - 17:15 GMT - Launch Vehicle: Pershing. FOT-143 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 February 17 - 17:51 GMT - Launch Vehicle: Pershing. FOT-142 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 February 17 - 19:17 GMT - Launch Vehicle: Pershing. FOT-144 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 April 7 - 14:00 GMT - Launch Vehicle: Pershing. FOT-146 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 April 7 - 14:19 GMT - Launch Vehicle: Pershing. FOT-147 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1981 April 7 - 14:40 GMT - Launch Vehicle: Pershing. FOT-148 Follow-on Test launch Agency: USA. Apogee: 250 km (150 mi).

1982 January 20 - 14:59 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 January 20 - 15:19 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 January 20 - 19:06 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 February 24 - 14:04 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 February 24 - 14:55 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 February 24 - 15:14 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 March 10 - 15:01 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 March 10 - 15:17 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 March 10 - 16:26 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1982 July 22 - 14:49 GMT - Launch Vehicle: Pershing. Pershing 2 1 FAILURE: Failure. Test mission Agency: USA?. Apogee: 1.00 km (0.60 mi).

1983 January 21 - 14:48 GMT - Launch Vehicle: Pershing. Pershing 2 3 Test mission Agency: USA. Apogee: 314 km (195 mi).

1983 February 9 - 15:06 GMT - Launch Vehicle: Pershing. Pershing 2 4 Test mission Agency: USA. Apogee: 342 km (212 mi).

1983 March 28 - 15:29 GMT - Launch Vehicle: Pershing. Pershing 2 7 Test mission Agency: USA. Apogee: 330 km (200 mi).

1983 April 10 - 19:55 GMT - Launch Vehicle: Pershing. Test mission Agency: USA. Apogee: 250 km (150 mi).

1983 May 27 - 14:48 GMT - Launch Vehicle: Pershing. Test mission Agency: USA. Apogee: 250 km (150 mi).

1983 June 2 - 14:46 GMT - Launch Vehicle: Pershing. Test mission Agency: USA. Apogee: 250 km (150 mi).

1983 July 27 - 14:15 GMT - Launch Vehicle: Pershing. Test mission Agency: USA. Apogee: 250 km (150 mi).

1983 September 7 - 17:04 GMT - Launch Vehicle: Pershing. Test mission Agency: USA. Apogee: 320 km (190 mi).

1983 September 23 - 12:05 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 September 23 - 13:21 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 September 23 - 14:34 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 September 23 - 14:55 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 September 23 - 16:17 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 October 13 - 16:25 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 October 13 - 16:50 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 October 13 - 17:13 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1983 October 13 - 17:43 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1984 May 16 - 14:31 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1984 August 7 - 12:00 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1984 September 20 - 14:30 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1984 October 3 - 14:22 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1985 December 16 - 13:03 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1985 December 17 - 16:02 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1985 December 17 - 21:37 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1986 June 24 - 13:56 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1986 June 24 - 15:23 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1986 June 24 - 16:33 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1986 June 26 - 13:05 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1986 June 26 - 16:47 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 March 24 - 13:33 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 March 24 - 13:52 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 March 24 - 14:13 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 March 24 - 15:34 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 March 24 - 15:54 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 March 24 - 16:17 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 May 21 - 02:00 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 May 21 - 02:19 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 May 21 - 02:40 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 May 21 - 04:00 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 May 21 - 04:33 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 May 21 - 04:51 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 July 27 - 12:38 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 July 27 - 12:57 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 July 27 - 15:20 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1987 July 27 - 15:37 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 January 13 - 14:01 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 February 15 - 13:03 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 February 15 - 13:21 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 February 15 - 13:42 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 February 15 - 15:16 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 February 15 - 15:42 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 February 15 - 16:01 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 March 21 - 13:01 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 March 21 - 13:19 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 March 21 - 14:13 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).

1988 March 21 - 15:45 GMT - Launch Vehicle: Pershing. Operational test Agency: USA. Apogee: 250 km (150 mi).