List of Atlas launches (1957–59)
Main article: List of Atlas launches
1957
Date/Time (UTC) |
Rocket | S/N | Launch Site | Payload | Function | Orbit | Outcome | Remarks |
---|---|---|---|---|---|---|---|---|
1957-06-11 19:37 |
Atlas A | 4A | CCAFS LC-14 | ICBM test | Suborbital | Failure | Maiden flight of Atlas A. Overheating in the boattail led to propulsion system failure. RSO T+50 seconds. | |
1957-09-25 19:57 |
Atlas A | 6A | CCAFS LC-14 | ICBM test | Suborbital | Failure | Overheating in the boattail led to propulsion system failure. RSO T+63 seconds. | |
1957-12-17 17:39 |
Atlas A | 12A | CCAFS LC-14 | ICBM test | Suborbital | Success |
1958
Date/Time (UTC) |
Rocket | S/N | Launch Site | Payload | Function | Orbit | Outcome | Remarks |
---|---|---|---|---|---|---|---|---|
1958-01-10 15:48 |
Atlas A | 10A | CCAFS LC-12 | ICBM test | Suborbital | Success | ||
1958-02-07 19:37 |
Atlas A | 13A | CCAFS LC-14 | ICBM test | Suborbital | Failure | Vernier feedback transducer short followed by propulsion system failure. Missile broke up T+164 seconds. | |
1958-02-20 17:46 |
Atlas A | 11A | CCAFS LC-12 | ICBM test | Suborbital | Failure | Vernier feedback transducer short followed by propulsion system failure. Missile broke up T+126 seconds. | |
1958-04-05 17:01 |
Atlas A | 15A | CCAFS LC-14 | ICBM test | Suborbital | Failure | Turbopump failure T+105 seconds. Missile remained structurally intact until impacting the ocean. | |
1958-06-03 21:28 |
Atlas A | 16A | CCAFS LC-12 | ICBM test | Suborbital | Success | Final flight of Atlas A | |
1958-07-19 17:36 |
Atlas B | 3B | CCAFS LC-11 | ICBM test | Suborbital | Failure | Maiden flight of Atlas B. Missile mistakenly launched with the gyroscope package powered off, leading to control failure and vehicle breakup at T+43 seconds. | |
1958-08-02 22:16 |
Atlas B | 4B | CCAFS LC-13 | ICBM test | Suborbital | Success | ||
1958-08-29 04:30 |
Atlas B | 5B | CCAFS LC-11 | ICBM test | Suborbital | Success | ||
1958-09-14 05:24 |
Atlas B | 8B | CCAFS LC-14 | ICBM test | Suborbital | Success | ||
1958-09-18 21:27 |
Atlas B | 6B | CCAFS LC-13 | ICBM test | Suborbital | Failure. | Turbopump failure T+80 seconds caused engine shutdown. Missile destroyed itself T+82 seconds. | |
1958-11-18 0400 |
Atlas B | 9B | CCAFS LC-11 | ICBM test | Suborbital | Failure | Partial failure. Excessive fuel consumption resulted in premature sustainer cutoff. | |
1958-11-29 02:27 |
Atlas B | 12B | CCAFS LC-14 | ICBM test | Suborbital | Success | ||
1958-12-18 23:02 |
Atlas B | 10B | CCAFS LC-11 | SCORE | Comsat | LEO | Success | First use of an Atlas vehicle for a space launch. |
1958-12-24 04:45 |
Atlas C | 3C | CCAFS LC-12 | ICBM test | Suborbital | Success | Maiden flight of Atlas C | |
1959
Date/Time (UTC) |
Rocket | S/N | Launch Site | Payload | Function | Orbit | Outcome | Remarks |
---|---|---|---|---|---|---|---|---|
1959-01-16 04:00 |
Atlas B | 13B | CCAFS LC-14 | ICBM test | Suborbital | Failure | Unexplained control and propulsion system difficulties (missile had no telemetry package) starting at T+100 seconds, followed by engine shutdown T+121 seconds. | |
1959-01-27 23:34 |
Atlas C | 4C | CCAFS LC-12 | ICBM test | Suborbital | Failure | Partial failure. Guidance system failed, however the flight control system kept the missile on course. Reentry vehicle not recovered. | |
1959-02-04 08:01 |
Atlas B | 11B | CCAFS LC-11 | ICBM test | Suborbital | Success | Final flight of Atlas B | |
1959-02-20 05:38 |
Atlas C | 5C | CCAFS LC-12 | ICBM test | Suborbital | Failure | Fuel staging disconnect valve failed to close at booster jettison, resulting in loss of tank pressure. Missile destroyed itself T+172 seconds. | |
1959-03-19 00:59 |
Atlas C | 7C | CCAFS LC-12 | ICBM test | Suborbital | Failure | Electrical glitches caused guidance system failure and premature booster engine shutdown, leading to unstable flight trajectory. RVX-2A reentry vehicle not recovered. | |
1959-04-14 21:46 |
Atlas D | 3D | CCAFS LC-13 | ICBM test | Suborbital | Failure | Maiden flight of Atlas D. Propellant leak at liftoff led to booster section explosion T+26 seconds. RSO T+35 seconds. | |
1959-05-19 04:30 |
Atlas D | 7D | CCAFS LC-14 | ICBM test | Suborbital | Failure | Pad hold-down arm malfunction damaged missile at liftoff, causing loss of tank pressure during ascent. Missile destroyed itself T+64 seconds. | |
1959-06-06 17:39 |
Atlas D | 5D | CCAFS LC-13 | ICBM test | Suborbital | Failure | Fuel staging disconnect valve failed to close at booster jettison, resulting in loss of tank pressure. Missile destroyed itself T+157 seconds. | |
1959-07-21 05:22 |
Atlas C | 8C | CCAFS LC-12 | ICBM test | Suborbital | Success | ||
1959-07-29 04:10 |
Atlas D | 11D | CCAFS LC-11 | ICBM test | Suborbital | Success | ||
1959-08-11 18:01 |
Atlas D | 14D | CCAFS LC-13 | ICBM test | Suborbital | Success | ||
1959-08-24 15:53 |
Atlas C | 11C | CCAFS LC-12 | ICBM test | Suborbital | Success | Final flight of Atlas C. RVX-1 reentry vehicle equipped with a camera package photographed the Earth and was recovered after a 250-mile suborbital lob. | |
1959-09-09 08:19 |
Atlas D | 10D | CCAFS LC-14 | Big Joe 1 | Mercury test | Suborbital | Failure. | Partial failure. Booster jettison failed due to bad electrical contacts. Boilerplate Mercury capsule successfully recovered. |
1959-09-09 17:50:42 |
Atlas D | 12D | VAFB LC-576A-2 | ICBM test | Suborbital | Success | First Atlas launch from Vandenberg | |
1959-09-17 02:09 |
Atlas D | 17D | CCASF LC-13 | ICBM test | Suborbital | Success | ||
1959-10-06 05:55 |
Atlas D | 18D | CCAFS LC-11 | ICBM test | Suborbital | Success | ||
1959-10-10 03:10 |
Atlas D | 22D | CCAFS LC-13 | ICBM test | Suborbital | Success | ||
1959-10-29 07:20 |
Atlas D | 26D | CCAFS LC-11 | ICBM test | Suborbital | Success | ||
1959-11-04 21:37 |
Atlas D | 28D | CCAFS LC-13 | ICBM test | Suborbital | Success | ||
1959-11-24 19:48 |
Atlas D | 15D | CCAFS LC-13 | ICBM test | Suborbital | Success | ||
1959-11-26 07:26 |
Atlas-Able | 20D | CCAFS LC-14 | Pioneer P-3 | Lunar probe | HEO (target) | Failure | Maiden flight of Atlas-Able. Payload fairing broke up at T+45 seconds, leading to loss of the upper stages and payload. Atlas performed normally. |
1959-12-09 00:10 |
Atlas D | 31D | CCAFS LC-13 | ICBM test | Suborbital | Success | ||
1959-12-19 00:48 |
Atlas D | 40D | CCAFS LC-13 | ICBM test | Suborbital | Success | First use of a "dry" engine start on an Atlas (igniter activated prior to propellant injection) | |
References
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