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Cape Canaveral LC17
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I think a future flight should include a poet, a priest and a philosopher � we might get a much better idea of what we saw.

   ---Collins

Cape Canaveral LC17
 
Launch Complex 17 Launch Site: Cape Canaveral. Launch Pads: 2. Latitude: 28.4465 N. Longitude: 80.5652 W. Delta, Delta 1000, Delta 2000, Delta 3, Delta 3000, Delta 4000, Delta 6000, Delta 7000, Delta A, Delta B, Delta C, Delta D, Delta E, Delta G, Delta L, Delta M, Delta N, Thor Able, Thor Able-Star, Thor DM-18, Thor DSV-2D, Thor DSV-2F, Thor DSV-2G.

This dual launch pad complex was built for the Thor ballistic missile program in 1956. Pad 17A supported its first Thor launch on 30 August 1957, and Pad 17B supported its first Thor launch on 25 January 1957. In addition to Thor missile launches, Complex 17 began supporting space launches in the late 1950s. The site was modified in the early 1960s to support a whole host of launch vehicles derived from the basic Thor booster. Thirty-five Delta missions were launched from Complex 17 between the beginning of 1960 and the end of 1965. Six ASSET (Aerothermodynamic/Elastic Structural Systems Environmental Test) launches were also conducted at Complex 17 between 18 September 1963 and 24 February 1965. The Air Force transferred Complex 17 to NASA in the spring of 1965, but the site was returned to the Air Force in October 1988 to support the Delta II program. As Delta II launches continued over the next decade, Pad 17B was modified in 1997 to support a new, more powerful launch vehicle - the Delta III. In all, Complex 17 supported 274 major missile and space launches between January 1957 and the end of October 1998.

  • 1957 Jan 26 - R&D; Series I Thor DM-18. Lox contamination, led to a valve failure. Thrust decayed, the booster settled back throught the thrust ring, causing an oxygen fire, followed by booster explosion.. Thor DM-18 101 Apogee: 0.000 km. First attempted test flight of USAF Thor IRBM, only 13 months after first production contracts were signed, failed to launch.
  • 1957 Apr 20 4:33 - R&D; Series I Thor DM-18. Console wiring error resulted in erroneous tracking indication; destroyed by range safety.. Thor DM-18 102 Apogee: 0.000 km.

    Douglas Thor IRBM (XSM-75) was launched at Cape Canaveral, Fla., destroyed by range safety officer. The missile was actually on course throughout its flight. The console wiring error led the range safety officer to believe it was headed inland rather than out to sea, so he hit the destruct button.

  • 1957 May 22 3:00 - R&D; Series I Thor DM-18. Stuck valve resulted in tank pressure buildup followed by booster explosion.. Thor DM-18 103 Apogee: 0.000 km.
  • 1957 Aug 30 - R&D; Series I Thor DM-18. Broke up after 92 seconds.. Thor DM-18 104 Apogee: 0.000 km.
  • 1957 Sep 20 - R&D; Series I Thor DM-18. Thor DM-18 105 Apogee: 520 km. Range: 1,800 km. Complete USAF Thor IRBM first successfully launched from Cape Canaveral. Dummy Warhead sent to 1800 km range.
  • 1957 Oct 3 17:13 - R&D; Series I Thor DM-18. Fell back on pad, followed by explosion.. Thor DM-18 107 Apogee: 0.000 km.
  • 1957 Oct 11 16:29 - R&D; Series I Thor DM-18. Turbopump gearbox failure.. Thor DM-18 108 Apogee: 520 km. Range: 2,780 km. Thor missile launched at Cape Canaveral, the second tested, achieved its designed 1,500-mile range.
  • 1957 Oct 24 16:32 - R&D; Series I Thor DM-18. Thor DM-18 109 Apogee: 520 km. Range: 4,400 km. Stripped down Thor long-range flight test successful from AMR, impacting 4400 km downrange.
  • 1957 Dec 7 22:11 - R&D; Series II Thor DM-18. Thor DM-18 112 Apogee: 520 km.
  • 1957 Dec 19 20:12 - R&D; Series II Thor DM-18. Thor DM-18 113 Apogee: 520 km. A Thor missile, the eighth tested and the fourth successfully, completed the first fully-guided Thor IRBM flight using an all-inertial guidance system.
  • 1958 Jan 28 - R&D; Series II Thor DM-18. Thor DM-18 114 Thor IRBM successfully fired from Cape Canaveral, flew prescribed course, and impacted in preselected area.
  • 1958 Feb 28 - R&D; Series II Thor DM-18. Failure. Thor DM-18 120 Apogee: 0.000 km. Copper heatsink nose cone
  • 1958 Apr 19 - R&D; Series II Thor DM-18. Failure. Thor DM-18 121 Apogee: 0.000 km.
  • 1958 Apr 23 - ARTV 1 (Able RTV) Thor Able. Thor turbopump gearbox failed T+150 sec.. Thor Able 116 Apogee: 0.000 km. Mouse 'Mia' not recovered.
  • 1958 Jun 13 - R&D; Series III Thor DM-18. Thor DM-18 122 Apogee: 520 km.
  • 1958 Jul 10 2:30 - ARTV 2 (Able RTV) Thor Able. Thor Able 118 Apogee: 1,600 km. Range: 9,600 km. Mouse 'Mia II' reached 1600 km altitude, flew 9600 km range, but re-entry vehicle not recovered.
  • 1958 Jul 13 - R&D; Series III Thor DM-18. Thor DM-18 123 Apogee: 520 km.
  • 1958 Jul 23 - ARTV 3 (Able RTV) Thor Able. Thor Able 119 Apogee: 1,600 km. Mouse 'Wickie' not recovered; nose cone lost.
  • 1958 Jul 26 - R&D; Series III Thor DM-18. Failure. Thor DM-18 126 Apogee: 0.000 km.
  • 1958 Aug 17 12:18 - Thor Able. Thor exploded after 77 sec.. Thor Able I 127 Apogee: 16 km.
  • 1958 Oct 11 8:42 - Thor Able. Third stage produced insufficient thrust. Partial Failure.. Thor Able I 130
  • 1958 Nov 5 - R&D; Series IV Thor DM-18. Thor DM-18A 138 Apogee: 520 km.
  • 1958 Nov 8 7:30 - Thor Able. Third stage ignition unsuccessful.. Thor Able I 129 Apogee: 1,550 km.
  • 1958 Nov 26 - R&D; Series IV Thor DM-18. Thor DM-18A 140 Apogee: 520 km. First operational launch
  • 1958 Dec 16 - R&D; Series IV Thor DM-18. Thor DM-18A 146 Apogee: 520 km.
  • 1959 Jan 23 - PGRTV 1 (RVX-1) Thor Able. First stage shut down at wrong time. Partial failure.. Thor Able II 128 Apogee: 0.000 km.
  • 1959 Jan 30 - R&D; Series IV Thor DM-18. Thor DM-18A 154 Apogee: 520 km.
  • 1959 Feb 28 - PGRTV 2 (RVX-1) Thor Able. Thor Able II 131 Apogee: 520 km. Inert 3rd stage
  • 1959 Mar 21 - PGRTV 3 (RVX-1) Thor Able. Thor Able II 132 Apogee: 520 km.
  • 1959 Mar 26 - R&D; Series IV Thor DM-18. Thor DM-18A 162 Apogee: 520 km.
  • 1959 Apr 8 - PGRTV 4 (RVX-1) Thor Able. Thor Able II 133 Apogee: 520 km.
  • 1959 Apr 23 - R&D; Series IV Thor DM-18. Thor DM-18A 176 Apogee: 520 km. Fourth recovery of a data capsule at AMR, USAF Thor 1,500-mile accuracy test flight.
  • 1959 May 12 - R&D; Series IV Thor DM-18. Thor DM-18A 187 Apogee: 520 km.
  • 1959 May 21 - PGRTV 5 (RVX-1) Thor Able. Thor Able II 135 Apogee: 520 km.
  • 1959 Jun 11 - PGRTV 6 (RVX-1) Thor Able. Thor Able II 137 Apogee: 520 km.
  • 1959 Jun 29 - R&D; Series IV Lofted Thor DM-18. Thor DM-18A 194 Apogee: 1,000 km.
  • 1959 Jul 21 - R&D; Series IV Thor DM-18. Failure. Thor DM-18A 203 Apogee: 0.000 km.
  • 1959 Aug 5 - R&D; Series IV Thor DM-18. Thor DM-18A 208 Apogee: 520 km.
  • 1959 Aug 7 14:24 - Thor Able. Thor Able III 134
  • 1959 Aug 27 - R&D; Series IV Thor DM-18. Thor DM-18A 216 Apogee: 520 km.
  • 1959 Sep 17 - Thor Able. Third stage failed.. Thor Able II 136
  • 1959 Sep 22 18:00 - R&D; Series IV Thor DM-18. Thor DM-18A 222 Apogee: 520 km.
  • 1959 Oct 13 - R&D; Series IV Thor DM-18. Thor DM-18A 221 Apogee: 520 km.
  • 1959 Nov 3 - R&D; Series IV Thor DM-18. Thor DM-18A 238 Apogee: 520 km.
  • 1959 Nov 19 - R&D; Series IV Thor DM-18. Thor DM-18A 244 Apogee: 520 km.
  • 1959 Dec 17 - R&D; Series IV Thor DM-18. Thor DM-18A 255 Apogee: 520 km.
  • 1960 Mar 11 13:00 - Thor Able. Thor Able IV 219
  • 1960 Apr 1 11:40 - Thor Able. Thor Able II 148
  • 1960 May 13 9:16 - Delta. Second stage attitude control failure.. Thor Delta 144/D1
  • 1960 Aug 12 9:39 - Delta. Thor Delta 270/D2
  • 1960 Aug 18 19:58 - Thor Able-Star. Exploded 2.5 minutes after launch.. Thor Ablestar 262 AB004?
  • 1960 Nov 23 11:13 - Delta. Thor Delta 245/D3
  • 1961 Mar 25 15:17 - Delta. Thor Delta 295/D4
  • 1961 Jul 12 10:25 - Delta. Thor Delta 286/D5
  • 1961 Aug 16 3:21 - Delta. Thor Delta 312/D6
  • 1962 Jan 15 11:07 - AVT-1 Thor DSV-2D. Thor DSV-2D 337 Apogee: 1,400 km.
  • 1962 Feb 8 12:43 - Delta. Thor Delta 317/D7
  • 1962 Mar 7 16:06 - Delta. Thor Delta 301/D8
  • 1962 Apr 26 18:00 - Delta. Thor Delta 320/D9
  • 1962 May 10 12:07 - Thor Able-Star. Able-Star failed to ignite.. Thor Ablestar 314 AB011
  • 1962 Jun 19 12:19 - Delta. Thor Delta 321/D10
  • 1962 Jul 10 8:35 - Delta. Thor Delta 316/D11
  • 1962 Jul 18 9:30 - AVT 2 Thor DSV-2D. Thor DSV-2D 338 Apogee: 1,484 km.
  • 1962 Sep 18 8:53 - Delta. Thor Delta 318/D12
  • 1962 Oct 2 22:11 - Delta A. Thor Delta A 345/D13
  • 1962 Oct 27 23:15 - Delta A. Thor Delta A 346/D14
  • 1962 Dec 13 23:30 - Delta B. Thor Delta B 355/D15
  • 1963 Feb 14 5:35 - Delta B. Thor Delta B 358/D16
  • 1963 Apr 3 2:00 - Delta B. Thor Delta B 357/D17
  • 1963 May 7 11:38 - Delta B. Thor Delta B 366/D18
  • 1963 Jun 19 9:50 - Delta B. Thor Delta B 359/D19
  • 1963 Jul 26 14:33 - Delta B. Thor Delta B 370/D20
  • 1963 Sep 18 9:40 - Asset 1 Thor DSV-2F. Thor DSV-2F 232 Apogee: 56 km.

    Suborbital test of subscale model of X-20 Dynasoar. Aero-thermodynamic structural test vehicle (ASV) for heat shield tests. Booster flew to peak altitude of 62 km, then pitched down, driving the spacecraft to separation at 59 km and 4,906 m/s. The spacecraft was sited under its parachute in the recovery zone at Ascension Island, but the flotation bag broke and it sank into the Atlantic.

  • 1963 Nov 27 2:30 - Delta C. Thor Delta C 387/D21
  • 1963 Dec 21 9:30 - Delta B. Thor Delta B 371/D22
  • 1964 Jan 21 21:14 - Delta B. Thor Delta B 373/D23
  • 1964 Mar 19 11:13 - Delta B. Insufficient third stage thrust.. Thor Delta B 391/D24
  • 1964 Mar 24 - Asset 2 Thor DSV-2G. Second stage fired, then shut down, repeating the sequence several times.. Thor DSV-2G 240 Apogee: 55 km. Range: 800 km.

    Suborbital test of subscale model of X-20 Dynasoar. Aero-thermodynamic structural test vehicle (ASV) for heat shield tests. Good first stage burn, but the second stage fired, then shut down, repeating the sequence several times. The spacecraft separated, and began to maneuver in a 60 degree bank to recover course, when the self-destruct package blew it apart. The debris impacted the Atlantic 800 km downrange near San Salvador Island.

  • 1964 Jul 22 - Asset 3 Thor DSV-2G. Thor DSV-2G 250 Apogee: 71 km.

    Suborbital test of subscale model of X-20 Dynasoar. Aero-thermodynamic structural test vehicle (ASV) for heat shield tests. Launched after four hours of holds. Tested Dynasoar hardware - tungsten nose cap, molbdenum panels with vapor-deposited disilicide, and liquid-cooled double-walled cockpit bathtub panel. Reached 5,500 m/s and recovered near Ascension Island 12 hours after launch.

  • 1964 Aug 19 12:15 - Delta D. Thor Delta D 417/D25
  • 1964 Oct 4 3:45 - Delta C. Thor Delta C 392/D26
  • 1964 Oct 28 - Asset 4 Thor DSV-2F. Thor DSV-2F 260 Apogee: 50 km. Range: 1,200 km.

    Suborbital test of subscale model of X-20 Dynasoar. Aero-environmental test vehicle (AEV) to test aerodynamic properties of flexing outer skin with corrugated columbium panel. Reached 4,000 m/s at 50.6 km altitude before being released from launch vehicle. Telemetry received for 900 seconds until spaceplane had reached Mach 2 1200 km downrange. It then became unstable and crashed into the Atlantic. Recovery was not planned.

  • 1964 Dec 9 - Asset 5 Thor DSV-2F. Thor DSV-2F 247 Apogee: 53 km. Range: 1,200 km.

    Suborbital test of subscale model of X-20 Dynasoar. Aero-environmental test vehicle (AEV) to test aerodynamic properties of flexing outer skin with corrugated columbium panel. Reached 4,000 m/s at 53.2 km altitude before being released from launch vehicle. Telemetry received for 900 seconds until spaceplane had reached Mach 2 1200 km downrange. It then became unstable and crashed into the Atlantic. Recovery was not planned.

  • 1964 Dec 21 9:00 - Delta C. Thor Delta C 393/D27
  • 1965 Jan 22 7:52 - Delta C. Thor Delta C 374/D28
  • 1965 Feb 3 16:36 - Delta C. Thor Delta C 411/D29
  • 1965 Feb 23 14:36 - Asset 6 Thor DSV-2G. Thor DSV-2G 248 Apogee: 70 km. Range: 4,350 km.

    Suborbital test of subscale model of X-20 Dynasoar. Reached 6,000 m/s and 4,350 km range. Tested twelve different kinds of refractory metals and covered with 2000 dots of heat-sensitive paint to characterize thermal profile on reentry. Telemetry indicated that the spacecraft survived reentry, but it evidently sank upon impacting the ocean and could not be recovered as planned.

  • 1965 Apr 6 23:47 - Delta D. Thor Delta D 426/D30
  • 1965 May 29 12:00 - Delta C. Thor Delta C 441/D31
  • 1965 Jul 2 4:07 - Delta C. Thor Delta C 415/D32
  • 1965 Aug 25 15:17 - Delta C. Premature third stage ignition.. Thor Delta C 434/D33
  • 1965 Nov 6 18:38 - Delta E. Thor Delta E 457/D34
  • 1965 Dec 16 7:31 - Delta E. Thor Delta E 460/D35
  • 1966 Feb 3 7:41 - Delta C. Thor Delta C 445/D36
  • 1966 Feb 28 13:58 - Delta E. Thor Delta E 461/D37
  • 1966 May 25 14:00 - Delta C. Thor Delta C1 436/D38
  • 1966 Jul 1 16:02 - Delta E. Thor Delta E1 467/D39
  • 1966 Aug 17 15:20 - Delta E. Thor Delta E1 462/D40
  • 1966 Oct 26 23:05 - Delta E. Partial Failure.. Thor Delta E1 464/D42
  • 1966 Dec 14 19:20 - Delta G. Thor Delta G 471/D43
  • 1967 Jan 11 10:55 - Delta E. Thor Delta E1 468/D44
  • 1967 Mar 8 16:12 - Delta C. Thor Delta C 431/D46
  • 1967 Mar 23 1:30 - Delta E. Thor Delta E1 470/D47
  • 1967 Jul 19 14:19 - Delta E. Thor Delta E1 488/D50
  • 1967 Sep 7 22:04 - Delta G. Thor Delta G 475/D51
  • 1967 Sep 28 0:45 - Delta E. Thor Delta E1 442/D52
  • 1967 Oct 18 15:58 - Delta C. Thor Delta C1 490/D53
  • 1967 Dec 13 14:08 - Delta E. Thor Delta E1 489/D55
  • 1968 Sep 19 0:09 - Delta M. Control system failure; destroyed by range safety.. Thor Delta M 529/D59
  • 1968 Nov 8 9:46 - Delta E. Thor Delta E1 479/D60
  • 1968 Dec 5 18:55 - Delta E. Thor Delta E1 481/D61
  • 1968 Dec 19 0:32 - Delta M. Thor Delta M 536/D63
  • 1969 Jan 22 16:48 - Delta C. Thor Delta C1 487/D64
  • 1969 Feb 6 0:39 - Delta M. Thor Delta M 530/D66
  • 1969 Feb 26 7:47 - Delta E. Thor Delta E1 483/D67
  • 1969 May 22 2:00 - Delta M. Thor Delta M 533/D68
  • 1969 Jun 29 3:15 - Delta N. Thor Delta N 539/D70
  • 1969 Jul 26 2:06 - Delta M. Third stage failure; left in unusable orbit.. Thor Delta M 547/D71
  • 1969 Aug 9 7:52 - Delta N. Thor Delta N 548/D72
  • 1969 Aug 27 21:59 - Delta L. Failure. Thor Delta L 540/D73
  • 1969 Nov 22 0:37 - Delta M. Thor Delta M 554/D74
  • 1970 Jan 15 0:16 - Delta M. Thor Delta M 557/D75
  • 1970 Mar 20 23:52 - Delta M. Thor Delta M 558/D77
  • 1970 Apr 23 0:46 - Delta M. Thor Delta M 559/D78
  • 1970 Jul 23 23:23 - Delta M. Thor Delta M 563/D79
  • 1970 Aug 19 12:11 - Delta M. Thor Delta M 561/D80
  • 1971 Feb 3 1:41 - Delta M. Thor Delta M 560/D82
  • 1971 Mar 13 16:15 - Delta M. Thor Delta M6 562/D83
  • 1971 Sep 29 9:45 - Delta N. Thor Delta N 565/D85
  • 1972 Sep 23 1:20 - Delta 1000. Delta 1604 579/D90
  • 1972 Nov 10 1:14 - Delta 1000. Delta 1914 580/D92
  • 1973 Apr 20 23:47 - Delta 1000. Delta 1914 583/D94
  • 1973 Jun 10 14:13 - Delta 1000. Delta 1913 581/D95
  • 1973 Oct 26 2:26 - Delta 1000. Delta 1604 582/D97
  • 1974 Jan 19 1:38 - Delta 2000. Partial Failure. Failed to reach planned orbit.. Delta 2313 587/D100
  • 1974 Apr 13 23:33 - Delta 2000. Delta 2914 588/D101
  • 1974 May 17 9:31 - Delta 2000. Delta 2914 590/D102
  • 1974 Oct 10 22:53 - Delta 2000. Delta 2914 589/D103
  • 1974 Nov 23 0:28 - Delta 2000. Delta 2313 591/D105
  • 1974 Dec 19 2:39 - Delta 2000. Delta 2914 599/D106
  • 1975 Feb 6 22:04 - Delta 2000. Delta 2914 593/D108
  • 1975 May 7 23:35 - Delta 2000. Delta 2914 596/D110
  • 1975 Jun 21 11:43 - Delta 1000. Delta 1910 586/D112
  • 1975 Aug 27 1:41 - Delta 2000. Delta 2914 594/D114
  • 1975 Oct 16 22:40 - Delta 2000. Delta 2914 597/D116
  • 1975 Nov 20 2:06 - Delta 2000. Delta 2910 604/D117
  • 1975 Dec 13 1:56 - Delta 3000. Delta 3914 607/D118
  • 1976 Jan 17 23:27 - Delta 2000. Delta 2914 606/D119
  • 1976 Feb 19 22:32 - Delta 2000. Delta 2914 603/D120
  • 1976 Mar 26 22:47 - Delta 3000. Delta 3914 610/D121
  • 1976 Apr 22 20:46 - Delta 2000. Delta 2914 608/D122
  • 1976 Jun 10 0:09 - Delta 2000. Delta 2914 601/D124
  • 1976 Jul 8 23:31 - Delta 2000. Delta 2914 611/D125
  • 1976 Oct 14 22:44 - Delta 2000. Delta 2914 614/D127
  • 1977 Jan 28 0:49 - Delta 2000. Delta 2914 613/D128
  • 1977 Mar 10 23:16 - Delta 2000. Delta 2914 612/D129
  • 1977 Apr 20 10:15 - Delta 2000. Delta 2914 617/D130
  • 1977 Jun 16 10:51 - Delta 2000. Delta 2914 616/D131
  • 1977 Jul 14 10:39 - Delta 2000. Delta 2914 618/D132
  • 1977 Aug 25 23:49 - Delta 2000. Delta 2313 615/D133
  • 1977 Sep 13 23:31 - Delta 3000. Failure.. Delta 3914 619/D134
  • 1977 Oct 22 13:53 - Delta 2000. Delta 2914 623/D135
  • 1977 Nov 23 1:35 - Delta 2000. Delta 2914 620/D136
  • 1977 Dec 15 0:47 - Delta 2000. Delta 2914 624/D137
  • 1978 Jan 26 17:36 - Delta 2000. Delta 2914 628/D138
  • 1978 Apr 7 22:01 - Delta 2000. Delta 2914 626/D140
  • 1978 May 11 22:59 - Delta 3000. Delta 3914 627/D141
  • 1978 Jun 16 10:49 - Delta 2000. Delta 2914 625/D142
  • 1978 Jul 14 10:43 - Delta 2000. Delta 2914 631/D143
  • 1978 Aug 12 15:12 - Delta 2000. Delta 2914 633/D144
  • 1978 Nov 19 0:46 - Delta 2000. Delta 2914 634/D146
  • 1978 Dec 16 0:21 - Delta 3000. Delta 3914 632/D147
  • 1979 Jan 30 21:42 - Delta 2000. Delta 2914 629/D148
  • 1979 Aug 10 0:20 - Delta 2000. Delta 2914 638/D149
  • 1979 Dec 7 1:35 - Delta 3000. Delta 3914 622/D150
  • 1980 Feb 14 15:57 - Delta 3000. Delta 3910 635/D151
  • 1980 Sep 9 22:27 - Delta 3000. Delta 3914 637/D152
  • 1980 Nov 15 22:49 - Delta 3000. Delta 3910/PAM 636/D153
  • 1981 May 22 22:29 - Delta 3000. Delta 3914 645/D154
  • 1981 Sep 24 23:09 - Delta 3000. Delta 3910/PAM 641/D156
  • 1981 Nov 20 1:37 - Delta 3000. Delta 3910/PAM 640/D158
  • 1982 Jan 16 1:55 - Delta 3000. Delta 3910/PAM 643/D159
  • 1982 Feb 26 0:04 - Delta 3000. Delta 3910/PAM 644/D160
  • 1982 Apr 10 6:47 - Delta 3000. Delta 3910/PAM 647/D161
  • 1982 Jun 9 0:24 - Delta 3000. Delta 3910/PAM 649/D162
  • 1982 Aug 26 23:10 - Delta 3000. Delta 3920/PAM 651/D164
  • 1982 Oct 28 1:28 - Delta 3000. Delta 3924 652/D165
  • 1983 Apr 11 21:39 - Delta 3000. Delta 3924 653/D167
  • 1983 Jun 28 23:08 - Delta 3000. Delta 3920/PAM D170
  • 1983 Jul 28 22:49 - Delta 3000. Delta 3920/PAM D171
  • 1983 Sep 22 22:16 - Delta 3000. Delta 3920/PAM D173
  • 1984 Sep 21 22:18 - Delta 3000. Delta 3920/PAM D176
  • 1986 May 3 22:18 - Delta 3000. Stage one main engine shutdown at T+71 seconds due to electrical failure.. Delta 3914 D178
  • 1987 Mar 20 22:22 - Delta 3000. Delta 3920/PAM D182
  • 1989 Mar 24 21:50 - Delta 3000. Delta 3920-8 D183
  • 1989 Aug 27 22:59 - Delta 4000. Delta 4925-8 D187
  • 1990 Feb 14 16:15 - Delta 6000. Delta 6920-8 D192
  • 1990 Apr 13 22:28 - Delta 6000. Delta 6925-8 D194
  • 1990 Jun 1 21:48 - Delta 6000. Delta 6920-10 D195
  • 1992 Jun 7 16:40 - Delta 6000. Delta 6920-10 D210
  • 1994 Feb 19 23:45 - Delta 7000. Delta 7925-8 D225
  • 1995 Aug 5 11:10 - Delta 7000. Partial Failure.. Delta 7925 D228
  • 1995 Dec 30 13:48 - Delta 7000. Delta 7920-10 D230
  • 1996 Feb 17 20:43 - Delta 7000. Delta 7925-8 D232
  • 1997 Jan 17 16:28 - Delta 7000. Launch failure.. Delta 7925 D241
  • 1997 Aug 25 14:39 - Delta 7000. Delta 7920-8 D247
  • 1998 Jan 10 0:32 - Delta 7000. Delta 7925-9.5 D252
  • 1998 Feb 14 14:34 - Delta 7000. Delta 7420-10C D253
  • 1998 Apr 24 22:38 - Delta 7000. Delta 7420-10C D256
  • 1998 Jun 10 0:35 - Delta 7000. Delta 7925-9.5 D258
  • 1998 Aug 27 1:17 - Delta 3. Due to guidance system induced oscillation all solid motor gimbal hydraulic fluid exhausted after only 71 seconds of flight. Range safety detroyed booster 75 seconds into flight at 16 km altitude.. Delta 8930 D259
  • 1998 Oct 24 12:08 - Delta 7000. Delta 7326-9.5 D261
  • 1998 Nov 22 23:54 - Delta 7000. Delta 7925-9.5 D263
  • 1998 Dec 11 18:45 - Delta 7000. Delta 7425-9.5 D264
  • 1999 Jan 3 20:21 - Delta 7000. Delta 7425-9.5 D265
  • 1999 Feb 7 21:04 - Delta 7000. Delta 7426-9.5 D266
  • 1999 May 5 1:00 - Delta 3. Engine failure at ignition for second burn of Centaur stage.. Delta 8930 D269
  • 1999 Jun 10 13:48 - Delta 7000. Delta 7420-10C D270
  • 1999 Jun 24 15:44 - Delta 7000. Delta 7320-10 D271
  • 1999 Jul 10 8:45 - Delta 7000. Delta 7420-10C D272
  • 1999 Jul 25 7:46 - Delta 7000. Delta 7420-10C D273
  • 1999 Aug 17 4:37 - Delta 7000. Delta 7420-10C D274
  • 1999 Oct 7 12:51 - Delta 7000. Delta 7925-9.5 D275
  • 2000 Feb 8 21:24 - Delta 7000. Delta 7420-10C D276
  • 2000 May 11 1:48 - Delta 7000. Delta 7925-9.5 D278
  • 2000 Jul 16 9:17 - Delta 7000. Delta 7925-9.5 D279
  • 2000 Aug 23 11:05 - Delta 3. Delta 8930 D280
  • 2000 Nov 10 17:14 - Delta 7000. Delta 7925-9.5 D281
  • 2001 Jan 30 7:55 - Delta 7000. Delta 7925-9.5 D283
  • 2001 Apr 7 15:02 - Delta 7000. Delta 7925-9.5 D284
  • 2001 May 18 17:45 - Delta 7000. Delta 7925-9.5 D285
  • 2001 Jun 30 19:46 - Delta 7000. Delta 7425-10 D286
  • 2001 Aug 8 16:13 - Delta 7000. Delta 7326-9.5 D287
  • 2002 Jul 3 6:47 - Delta 7000. Delta 2-7425-9.5/Star 30
 
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Last update 9 August 2003.

© Mark Wade, 2003 .








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