Name |
General Mission |
Launch Vehicle (Site) |
Performance Veh |
Performance Payload |
Performance Mission Results |
November 16, 1962 |
Saturn (SA-3) |
Launch vehicle development test ("Project Highwater") |
Saturn C-1 (AMR) |
S |
S |
S |
December 16 |
Explorer XVI (S-55b) |
Scientific micrometeoroid satellite |
Scout (WS) |
S |
S |
S |
March 28, 1963 |
Saturn (SA-4) |
Launch vehicle development test ("engine out" capability test) |
Saturn C-1 (AMR) |
S |
S |
S |
April 2 |
Lunik IV |
Lunar probe-reported attempt to soft-land instrument package |
Unknown (U.S.S.R) |
Unknown |
Unknown |
Unknown |
April 2 |
Explorer XVII |
Measure atmospheric density, composition, pressure, and temperature at altitudes of 249 to 933 kilometers (155 to 580 miles) |
Thor-Delta (AMR) |
S |
S |
S |
May 15 |
Faith 7 (MA-9) |
Project Mercury manned one-day mission-fourth US manned orbital flight |
Atlas (AMR) |
S |
S |
S |
June 14 |
Vostok V |
Manned orbital space flight. First launch of second tandem flight |
Unknown (U.S.S.R.) |
S |
S |
S |
June 16 |
Vostok VI |
Manned orbital space flight. Second launch of second tandem flight |
Unknown (U.S.S.R.) |
S |
S |
S |
July 20 |
|
Experimental heatshield reentry (29,934 kilometers per hour) (18,600mph) test |
Scout (WS) |
F |
F |
F |
August 28 |
|
Prove capability of Little Joe II as an Apollo spacecraft test vehicle |
Little Joe II (WSMR) |
S |
S |
S |
November 7 |
Pad Abort-1 |
Qualification test of Apollo launch escape system to effect a safe pad abort. (Spacecraft BP-6) |
(WSMR) |
- |
S |
S |
November 26 |
Explorer XVIII |
To measure interplanetary magnetic fields, solar wind, and cosmic radiation between earth and moon |
Thor-Delta (AMR) |
S |
S |
S |
November 27 |
Centaur II |
In-space ignition of Centaur's liquid-hydrogen engines (second attempt, first success) |
Atlas-centaur (AMR) |
S |
S |
S |
December 19 |
Explorer XIX |
To measure atmospheric density fluctuations of earth's high latitudes |
Scout (PMR) |
S |
S |
S |
January 29, 1964 |
Saturn (SA-5) |
Test structure and performance of 2-stage Saturn; orbit second stage |
Saturn I (AMR) |
S |
S |
S |
January 30 |
Ranger VI |
Television photographs of moon at close range |
Atlas-Agena B (AMR) |
S |
F |
F |
April 8 |
Gemini-Titan 1 |
Unmanned flight test of structural integrity of Gemini spacecraft and compatibility with launch vehicle |
Titan II (AMR) |
S |
S |
S |
April 14 |
Project Fire |
Test of Apollo sample heatshield material at lunar reentry speeds |
Atlas D (AMR) |
S |
S |
S |
May 13 |
Apollo Mission A-001 |
Test capability of launch escape system to propel spacecraft from launch vehicle during abort at transonic speed (Spacecraft BP-12) |
Little Joe II (WSMR) |
S |
S |
S |
May 28 |
Apollo Mission A-101 (SA-6) |
First flgiht of an Apollo-configured spacecraft with a Saturn launch vehicle (Spacecraft BP-13) |
Saturn I (AMR) |
S |
S |
S |
July 28 |
Ranger VII |
Television photographs of the moon at close range |
Atlas-Agena B (AMR) |
S |
S |
S |
August 18 |
|
Experimental heatshield reentry test |
Scout (WS) |
S |
S |
S |
August 25 |
Explorer XX |
Map irregularities in topside of earth's atmosphere; obtain electron densities and temperatures near satellite |
Scout (PMR) |
S |
S |
S |
September 18 |
Apollo Mission A-102 (SA-7) |
Demonstrate spacecraft-launch vehicle compatibility (Spacecraft BP-15) |
Saturn I (AMR) |
S |
S |
S |