| astronautix.com | October 18 |
1947 - Nation: USSR. Launch Vehicle: V-2.
Range achieved 206.7 km. Destroyed during ballistic portion of flight. References: 283 , 344 .
1954 - Nation: USA. Launch Vehicle: Saturn C-3BN, Saturn C-5N, Saturn I RIFT.
At the suggestion of Theodore von Kármán and following a request of Gen. H. B. Thatcher, an Ad Hoc Committee of the Scientific Advisory Board met in the Pentagon to consider the application of nuclear energy to missile propulsion. In its report, the Committee "noted that there was an almost complete hiatus in the study of the nuclear rocket from 1947 following a report by North American Aviation, until a 1953 report by the Oak Ridge National Laboratory. Because the technical problems appear so severe, and because another 6 years of no progress in this area would seem to be unfortunate," the Committee felt that a continuing study both analytical and experimental, at a modest level of effort, should be carried on. References: 17 .
1955 - Nation: USA. Launch Site: White Sands . Launch Vehicle: Aerobee. LV Configuration: RTV-N-10c.
Solar spectrum research. Launched at 1549 local time. Reached 150 km.
1956 - - 09:05 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC6. Launch Vehicle: Jupiter A. LV Configuration: Redstone s/n CC-14.
CC-14 was launched at 0405 hours EST from AMR after a series of short holds. The flight was successful. The actual range was 137.870 nm; 72 meters over and 338 meters right: of the intended impact point. The primary objectives were to test the accuracy of the guidance system and to test angle of-attack meters for the Jupiter. Missed aimpoint by 346 m. References: 439 .
1960 - Nation: USA. Launch Vehicle: Iris.
Second Iris rocket rose to 140 miles with a payload of 125 pounds from Wallops Station. References: 17 .
1962 - - 16:59 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC12. Launch Vehicle: Atlas LV-3A / Agena B. LV Configuration: Atlas s/n 215D / Agena B s/n 6005 (AA7).
The Ranger V lunar probe was launched from Atlantic Missile Range by an Atlas-Agena B launch vehicle. The Agena B stage attained parking orbit and 25 minutes later reignited to send Ranger V toward the moon. A malfunction in the Agena B guidance system resulted in excessive spacecraft velocity. The spacecraft's solar cells did not provide power and reversed command signals caused the telemetry antenna to lose earth acquisition. This made reception of the flight-path correction signal impossible and rendering its television cameras useless. Reversed command signals caused the telemetry antenna to lose earth acquisition, and mid-course correction was not possible. The spacecraft missed the Moon by 725 km and went into solar orbit. Gamma-ray data were collected for 4 hours prior to the loss of power. Ranger V was to have relayed television pictures of the lunar surface and rough-landed an instrumented capsule containing a seismometer. The spacecraft was tracked for 8 hours, 44 minutes, before its small reserve battery went dead. Additional Details: Ranger 5. References: 1 , 2 , 5 , 6 , 16 , 278 , 296 .
1963 - - 09:30 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Vostok 8A92.
Area survey photo reconnaissance satellite. References: 1 , 2 , 5 , 6 , 93 .
1967 - - 13:26 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: R-36-O.
Fractional Orbital Bombardment system test. Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 .
1969 - - 10:00 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC133/1. Launch Vehicle: Kosmos 11K63.
Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 , 99 .
1972 - - 12:00 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Voskhod 11A57.
Area survey photo reconnaissance satellite; returned film capsule; separated Nauka autonomous subsatellite 16KS No 161 / 1L which tested Kondor control system for Yantar satellite. References: 1 , 2 , 6 , 69 .
1974 - - 15:07 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Voskhod 11A57.
High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 1 , 2 , 6 .
1984 - - 17:31 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC32. Launch Vehicle: Tsyklon 3.
Replaced Cosmos 1455. References: 1 , 2 , 5 , 6 .
1989 - Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC39B. Launch Vehicle: Shuttle. LV Configuration: STS-70.
Atmospheric probe; deployed from Galileo 7/13/95; entered Jupiter atmosphere 12/7/95. Entry into Jupiter Dec 7 References: 2 , 5 , 6 .
Manned five crew. Deployed Galileo .Payloads: Deploy IUS with Galileo spacecraft. Shuttle Solar Backscatter Ultraviolet (SSBUV), Polymer Morphology (PM) experiments, IMAX camera project, Mesoscale Lightning Experiment (MLE), Air Force Maui Optical Site (AMOS) experiment, Growth Hormone Concentration and Distribution (GHCD) in Plants experiment, Sensor Technology Experiment (STEX), SSIP Student Experiment (SE) 82-15, Ice Crystals Experiment. First flight at this inclination. Additional Details: STS-34. References: 1 , 2 , 5 , 6 , 7 .
Deployed from STS-34 10/18/89; entered Jupiter orbit 12/7/95; investigations of Jupiter's moons, atmosphere, magnetosphere; antenna failed to deploy. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 1 , 2 , 5 , 6 .
1993 - - 14:53 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC39B. Launch Vehicle: Shuttle. LV Configuration: STS-58.
Biological, microgravity experiments aboard Spacelab 2. Payloads: Spacelab Life Sciences (SLS) 2, Shuttle Amateur Radio Experiment (SAREX) II. Additional Details: STS-58. References: 1 , 2 , 5 , 6 , 7 .
1999 - - 13:22 GMT. Nation: USA. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U / Ikar. LV Configuration: Soyuz 11A511U / Ikar s/n ST05.
At the time of this launch Globalstar began limited service of its satellite telephone system.
2000 - Nation: USA.
Jeff Wisoff and Mike Lopez-Alegria each jetted slowly through space above Discovery's cargo bay, demonstrating the small rescue nitrogen powered SAFER backpack (Simplified Aid for EVA Rescue). This would be used in the future to help a drifting astronaut regain the safety of the spacecraft. Each astronaut performed one 15 meter flight with the SAFER while attached to the shuttle with a long tether. Lopez-Alegria and Wisoff, with Koichi Wakata operating the arm, also completed a series of wrap-up tasks during the EVA. They removed a grapple fixture from the Z1 truss, opened and closed a latch assembly that will hold the solar array truss when it arrives, deployed a tray that will be used to provide power to the U.S. Laboratory Destiny, and tested the manual berthing mechanism latches that will support Destiny. Wisoff opened and closed the latches on the capture assembly for the P6 solar arrays using a pistol grip tool. With it he made more than 125 turns to open the latches, then closed and reopened them. He left the capture latch, called 'the claw,' ready to receive the solar arrays, to be installed by the STS-97 crew. An exercise to test techniques for returning an incapacitated astronaut to the air lock was cancelled because of time constraints.