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 starting at T+100 seconds, followed by engine shutdown T+121 seconds. No T/M aboard missile.
|
1959-01-27 23:34
|
Atlas C
|
4C
|
CCAFS LC-12
|
|
ICBM test
|
Suborbital
|
Partial failure
|
Guidance system failure T+80 seconds, 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. LOX fill/drain valve failed to close at liftoff, leading to booster section explosion T+26 seconds. RSO T+36 seconds.
|
1959-05-19 04:30
|
Atlas D
|
7D
|
CCAFS LC-14
|
|
ICBM test
|
Suborbital
|
Failure
|
Launcher 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
|
Partial failure
|
Booster jettison failed due to bad electrical contacts. Planned range not achieved. 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
|
CCAFS 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
|
Partial failure
|
One vernier shut down at staging due to a ruptured LOX duct. Roll control lost, missile impacted short of its intended range.
|
1959-11-04 21:37
|
Atlas D
|
28D
|
CCAFS LC-13
|
|
ICBM test
|
Suborbital
|
Partial failure
|
Short in impact predictor system leads to Range Safety Officer issuing erroneous manual cutoff command T+274 seconds. Missile impacted short of its intended range.
|
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)
|