| astronautix.com | June 11 |
1928 - Nation: Germany. Launch Vehicle: Me-163.
Friedrich Stamer made first manned rocket-powered flight in a tailless glider from the Wasserkuppe in the Rhön Mountains of Germany. Takeoff was made by elastic launching rope assisted by 44-pound thrust rocket, another rocket was fired while airborne, and a flight of about 1 mile was achieved. This flight was a part of experimentation directed by A. Lippisch. References: 17 .
1930 - Nation: Russia.
1940 - Nation: USA. Launch Vehicle: Goddard P-C.
Static test, steadier run 43.5 sec, longest to date; red-hot stones seen to fly up out of cement gas deflector. References: 482 .
1944 - Nation: USA.
1948 - Nation: USA. Launch Site: White Sands . Launch Complex: LC33. Launch Vehicle: V-2. LV Configuration: V-2 number 37.
Launched 03:22 local time. Reached 62.4 km. Carried pressure, temperature, composition, ionosphere, sky brightness, solar radiation experiments for Air Research and Development Command. Also carried Albert, the first American primate in space, who died of suffocation.
1948 - Nation: USSR.
Council of Soviet Ministers (SM) Decree 2018-791 'On construction of a test site to ground-test rocket engines.' was issued. References: 474 .
1951 - Nation: USA. Launch Site: Edwards .
Navy D-558-II Douglas Sky-rocket, flown by test pilot William Bridgeman, set a new unofficial airplane speed and altitude record at Edwards AFB, Muroc Dry Lake, Calif.; speed estimated at more than 1,200 mph; altitude estimated 70,000 feet. References: 17 .
1957 - Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: R-7 8K71. LV Configuration: R-7 8K71 M1-6.
After third attempt in three days to launch R-7 8K71 M1-6, the rocket is pulled from the pad. It is found that a nitrogen scavenging valve was installed backwards.
1957 - Nation: USA. Launch Vehicle: Atlas A. LV Configuration: Atlas 4A.
First test flight of prototype WS-107A Atlas was detonated by command signal at 10,000 feet following a failure in the booster fuel system. References: 17 , 278 .
1958 - Nation: USSR. Launch Site: Kapustin Yar . Launch Vehicle: Burya. LV Configuration: Burya s/n 3/1.
Cruise stage tanks 2 and 3 and engine feed tank all filled with fuel. Tanks 1 and 4 were empty. The AVD Engine Cutoff System activated at T+6 seconds due to a problem in one of the chambers of the boosters. Launch did not occur.
1958 - - 01:59 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC6. Launch Vehicle: Jupiter A. LV Configuration: Redstone s/n CC-48. FAILURE: Human error - thrust controller not connected.
Successfully fired at 2059 hours EST from AMR. The flight was a success in that all missions were accomplished with the exception of failure of the thrust governor. This failure was caused by human error before firing which caused excess velocity, thereby exceeding the predicted impact point by 8.36 nm. Programmed range to impact was 137.31 nm. All other missions were satisfactorily completed. Missed aimpoint by 14,917 m. References: 439 .
1959 - Nation: USA. Launch Site: Cape Canaveral . Launch Vehicle: Thor Able. LV Configuration: Thor-DM18 / Able-2.
Suborbital. References: 5 .
1960 - Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC11. Launch Vehicle: Atlas D. LV Configuration: Atlas 54D.
1962 - Nation: Russia.
1968 - Nation: USA.
Maximum Speed - 697 kph. Maximum Altitude - 13720 m. Flight Time - 246 sec. References: 49 , 97 .
1970 - Nation: USA.
Glide landing study. Maximum Speed - 809 kph. Maximum Altitude - 13716 m. Flight Time - 202 sec. References: 49 , 97 .
1971 - - 10:04 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Voskhod 11A57.
High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 1 , 2 , 6 .
1976 - Nation: USSR. Launch Vehicle: Energia.
Decree 'On selection of design layout for Buran' was issued. Following exhaustive analysis and inability to improve on the design, a straight aerodynamic copy of the US space shuttle, was selected as the Buran orbiter configuration. MiG was selected as subcontractor to build the orbiter. For this purpose MiG spun off a new design bureau, Molniya, with G E Lozino-Lozinskiy as chief designer. References: 474 .
1984 - - 08:38 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
Military cartographic satellite; returned film capsule. References: 1 , 2 , 6 .
1985 - - 14:38 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC41/1. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / 2BL.
Replaced Cosmos 1481. Covered Oko constellation plane 6 - 114 degree longitude of ascending node. References: 1 , 2 , 5 , 6 , 100 .
1986 - Nation: USSR. Launch Site: Baikonur . Launch Complex: Jubilee.
Maximum speed 530 kph. Maximum altitude 4000 m. Time 22 minutes. References: 81 .
1986 - - 07:55 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
Military cartographic satellite; returned film capsule. Also investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. References: 1 , 2 , 6 .
1988 - - 10:04 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
Military cartographic satellite; returned film capsule. References: 1 , 2 , 6 .
1991 - - 05:45 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 47159-819.
1999 - - 17:15 GMT. Nation: USA. Launch Site: Taiyuan . Launch Complex: LC1. Launch Vehicle: CZ-2C/SD. LV Configuration: CZ-2C/SD s/n CZ2C-21.