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April 2
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See also Born on this Day On this day in: 1946 - Launch Vehicle: Atlas A, MX-774.
1948 - 13:47 GMT - Launch Site: White Sands. Launch Complex: LC33. Launch Vehicle: V-2. LV Configuration: V-2 25. -
V-2 Aeronomy/Ionosphere mission Nation: USA. Agency: USA. Apogee: 144 km (89 mi). Launched 06:40 local time. Reached 144.4 km. Carried Density, pressure, temperature, composition, cosmic and solar radiation (Naval Research Lab) experiments for Signal Corps Engineering Lab, University of Michigan.
1953 - Launch Site: Kapustin Yar. Launch Vehicle: R-5. -
R-5 Phase I state trials launch Nation: USSR. Agency: NII-88. Apogee: 300 km (180 mi).
1958 - -
Eisenhower proposed the establishment of NASA Nation: USA. President Dwight D. Eisenhower, in a message to Congress, proposed the establishment of a National Aeronautics and Space Agency into which the National Advisory Committee for Aeronautics would be absorbed. The new agency would conduct the civilian space program through research in its own facilities or by contract and would also perform military research required by DOD. Projects primarily military in character would remain the responsibility of DOD. - Additional details.
1959 - -
Seven astronauts selected for Mercury project. Nation: USA. Program: Mercury. Class: Manned. Type: Spacecraft. Spacecraft: Mercury. Seven astronauts were selected for Project Mercury after a series of the most rigorous physical and mental tests ever given to U.S. test pilots. Chosen from a field of 110 candidates, the finalists were all qualified test pilots: Capts. Leroy G. Cooper, Jr., Virgil I. Grissom, and Donald K. Slayton, (USAF); Lt. Malcolm S. Carpenter, Lt. Comdr. Alan B. Shepard, Jr., and Lt. Comdr. Watler M. Schirra, Jr. (USN); and Lt. Col. John H. Glenn (USMC).
1959 - -
Bidders briefing for Project Mercury worldwide tracking range Nation: USA. Program: Mercury. A preliminary briefing was conducted for prospective bidders on construction of the worldwide tracking range for Project Mercury. This meeting was attended by representatives from 20 companies. At this time the preliminary plan called for an orbital mission tracking network of 14 sites. Contacts had not been made with the governments of any of the proposed locations with the exception of Bermuda. It was planned that all the sites would have facilities for telemetry, voice communications with the pilot, and teletype (wire or radio) communications with centers in the United States for primary tracking. The tracking sites would provide the control center at Cape Canaveral, Florida, with trajectory predictions; landing-area predictions; and vehicle, systems, and pilot conditions.
1959 - -
NASA Astronaut Training Group 1 selected. Nation: USA. The group was selected to provide six pilots for the single-crew Mercury manned spacecraft. Originally a wide pool of candidates was going to be considered, but in December 1958 President Eisenhower ruled that military test pilots would form the candidate pool.. Qualifications: Qualified jet pilot with minimum 1,500 flight-hours/10 years experience, graduate of test pilot school, bachelor's degree or equivalent, under 40 years old, under 180 cm height, excellent physical condition.. Screening of military service records showed 110 military officers that met these criteria. These 110 were to be called in three groups for briefings on the Mercury program. Of the first two groups of 35 called, 56 volunteered for further physical and psychiatric tests. This provided enough candidates and the third group was never even called for a briefing or asked if they would like to volunteer. Of the 56 tested, seven were finally selected (no objective way was found to reduce the seven finalists to six).
Of the seven astronauts, all eventually flew in space. Grounded due to a heart murmur, Slayton had to wait 16 years for his flight aboard the last Apollo mission. Glenn left for a career in politics after becoming the first American to orbit the earth, but returned to space aboard a shuttle over 36 years later in a NASA publicity stunt. Schirra was the only astronaut to fly aboard Mercury, Gemini, and Apollo spacecraft. Shepard was the only one to reach the lunar surface (after being grounded for a medical condition during the Gemini program). Grissom would die in the Apollo 204 ground fire.
1961 - 14:06 GMT - Launch Site: Baikonur. Launch Complex: LC41. Launch Vehicle: R-16. LV Configuration: R-16 5L-7T.
1963 - -
Final contract with McDonnell for the Gemini spacecraft. Nation: USA. Program: Gemini. Spacecraft: Gemini. NASA announced the signing of a contract with McDonnell for the Gemini spacecraft. Final negotiations had been completed February 27, 1963. Estimated cost was $428,780,062 with a fixed fee of $27,870,000 for a total estimated cost-plus-fixed-fee of $456,650,062. NASA Headquarters spent two weeks on a detailed review of the contract before signing. Development of the spacecraft had begun in December 1961 under a preliminary letter contract which the final contract superseded. The contract call for a 13 flight-rated spacecraft, 12 to be used in space flight, one to be used for ground testing. In addition, McDonnell would provide two mission simulator trainers, a docking simulator trainer, five boilerplates, and three static articles for vibration and impact ground tests.
1963 - 08:16 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1. Launch Vehicle: Molniya 8K78. Model: Molniya 8K78/E6. LV Configuration: Molniya 8K78/E6 G103-11. -
Luna 4 Nation: USSR. Program: Luna. Payload: E-6 s/n 3. Mass: 1,422 kg (3,134 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna E-6. Agency: RVSN. Perigee: 167 km (103 mi). Apogee: 182 km (113 mi). Inclination: 64.70 deg. Period: 87.98 min. COSPAR: 1963-008A. USAF Sat Cat: 563. Decay Date: 1963-04-03. Luna 4 was the second attempted Soviet unmanned lunar soft lander probe. The spacecraft, rather than being sent on a straight trajectory toward the Moon, was placed first in an earth parking orbit. The rocket stage then reignited and put the spaccecraft on a translunar trajectory. Failure of Luna 4 to make a required midcourse correction resulted in it missing the Moon by 8336.2 km on April 6, at 4:26 a.m. Moscow time. It thereafter entered a barycentric Earth orbit. The Soviet news agency, Tass, reported that data had been received from the spacecraft throughout its flight and that radio communication would continue for a few more days.
1964 - Launch Site: San Marco. Launch Complex: Rita. Launch Vehicle: Nike Apache. -
Nike Apache Test mission Nation: Italy. Agency: CRA. Apogee: 200 km (120 mi).
1964 - 02:42 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1. Launch Vehicle: Molniya 8K78M. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M T15000-23.
1965 - 13:22 GMT - Launch Complex: CVE-25 U. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.185UE.
1966 - Launch Site: Baikonur. Launch Complex: PU31. Launch Vehicle: R-36. Model: R-36 8K67. -
R-36 SLI K Operational Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1968 - -
40 percent nitrogen for the Apollo CM cabin in prelaunch operations Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NASA Hq. confirmed oral instructions to MSC and KSC to use 60 percent oxygen and 40 percent nitrogen to pressurize the Apollo CM cabin in prelaunch checkout operations and during manned chamber testing, as recommended by the Design Certification Review Board on March 7 and confirmed by the NASA Administrator on March 12. This instruction was applicable to flight and test articles at all locations.
1968 - Launch Site: Vandenberg. Launch Complex: 395. Launch Pad: 395-C. Launch Vehicle: Titan 2. Model: Titan II. LV Configuration: Titan 2 s/n M68B-36 / 62-0017.
1969 - Launch Site: Baikonur. Launch Complex: LC162. Launch Pad: LC162/36. Launch Vehicle: R-36. Model: R-36 8K67. -
R-36 OT? operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1969 - 08:32 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. -
MR-12 Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 181 km (112 mi).
1969 - 10:33 GMT - Launch Site: Baikonur. Launch Complex: LC81. Launch Pad: LC81/24. Launch Vehicle: Proton 8K82K / 11S824. Model: Proton-K/D. LV Configuration: Proton-K/D 233-01. FAILURE: First stage - 1 x RD-253 fire beginning at T+ 0.02 sec, rocket crashed near pad. -
M-69 s/n 522 Nation: USSR. Program: Mars. Payload: M-69 s/n 522. Class: Planetary. Type: Mars. Spacecraft: Mars M-69. Agency: RVSN. COSPAR: F690402A. Decay Date: 1969-04-02. Mars probe intended to enter Martian orbit and comprehensively photograph Mars, together with a landing probe. Further Mars launches during the 1969 launch window were cancelled when this attempt resulted in a major accident, which almost wiped out all of the leaders of the space industry. The Proton rocket lifted off, but one engine failed. The vehicle flew at an altitude of 50 m horizontally, finally exploding only a short distance from the launch pad, spraying the whole complex with poisonous propellants that were quickly spread by the wind. Everyone took off in their autos to escape, but which direction to go? Finally it was decided that the launch point was the safest, but this proved to be even more dangerous - the second stage was still intact and liable to explode. The contamination was so bad that there was no way to clean up - the only possibility was just to wait for rain to wash it away. This didn't happen until the Mars launch window was closed, so the first such probe was not put into space until 1971. This accident also severely damaged plans to divert attention from America's Apollo programme during the rest of 1969. 10-12 UR-500K launches had been intended to land on the moon lunar soil return and rover robots to supplement the N1 launches.
1970 -
1970 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-309. -
Minuteman 3 Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1970 - 01:46 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S66/1. -
Skylark ESRO S66/1 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 198 km (123 mi).
1971 - -
International Delegations tour Star City. Nation: USSR. Star City staff is busy preparing for foreign delegations attending the communist party congress that will also visit the cosmonaut centre. There is dirty snow, icy roads - and in two days 100 delegates will have to get to the forested location and be able to get around. The Vietnamese are coming on 4 April, followed by the Hungarians on 6 April and the Czechs on 7 April. A standard tour is laid out, to be followed by the films 'Our Gagarin' and 'In Memory of a Visit to Star City'.
1971 - 08:20 GMT - Launch Site: Plesetsk. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57.
1971 - 10:40 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12. -
MR-12 Aeronomy/Ionosphere mission Nation: USSR. Apogee: 150 km (90 mi).
1974 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Vehicle: Minuteman 2. -
Minuteman 2 FOT GT119M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).
1975 - 11:00 GMT - Launch Site: Baikonur. Launch Complex: LC90. Launch Pad: LC90. Launch Vehicle: Tsyklon 2. Model: Tsiklon-2.
1976 - -
Crew escape system test sled on dock, Downey Nation: USA. Program: STS.
1976 - Launch Site: Wallops Island. Launch Vehicle: Athena. LV Configuration: Athena Athena D. -
Athena MSV-1 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).
1980 - 12:39 GMT - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4. -
Trident C-4 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1980 - 14:23 GMT - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4. -
Trident C-4 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1980 - 14:23 GMT - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4. -
Trident C-4 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1981 - Launch Site: Wallops Island. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.20GE. -
Taurus Orion Plasma mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1982 - 10:15 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
1983 - 02:02 GMT - Launch Site: Baikonur. Launch Vehicle: Molniya 8K78M. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M ML.
1984 - 07:15 GMT - Launch Site: Poker Flat. Launch Vehicle: Taurus Nike Tomahawk TNT. Model: Taurus Nike Tomahawk. LV Configuration: Taurus Nike Tomahawk NASA 38.01UE. -
Taurus Nike Tomahawk TNT Plasma mission Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).
1984 - 07:17 GMT - Launch Site: Poker Flat. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.42UE. -
Taurus Orion Plasma mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1987 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Vehicle: Minuteman 3. -
Minuteman 3 IPMS Re-entry Vehicle Test mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1988 - Launch Site: Baikonur. Launch Complex: Jubilee.
1989 - 02:28 GMT - Launch Site: Kourou. Launch Complex: ELA1. Launch Pad: ELA1. Launch Vehicle: Ariane 2/3. Model: Ariane 2. LV Configuration: Ariane 2 V30. -
TELE-X Nation: Sweden. Program: TELE. Payload: Tele X. Mass: 2,142 kg (4,722 lb). Class: Communications. Spacecraft: Spacebus 300. Agency: NSAB. Perigee: 36,061 km (22,407 mi). Apogee: 36,128 km (22,448 mi). Inclination: 4.30 deg. Period: 1,451.80 min. COSPAR: 1989-027A. USAF Sat Cat: 19919. Completed Operations Date: 1998-01-13. TV, business communications for Nordic countries; 5 deg E. High power telecommunications satellite with a dual mission; direct TV broadcasting and data communications. Four active transponders with two redundant; power output 200 W per transponder. Coverage area - East Nordic coverage zone as defined by ITU (WARC -77). Mission period estimated to be 6 to 8 years. Position 5 deg E. Positioned in geosynchronous orbit at 5 deg E in 1989-1998 As of 28 August 2001 located at 138.62 deg W drifting at 3.929 deg W per day. As of 2007 Mar 10 located at 132.37W drifting at 3.933W degrees per day.
1992 - 01:50 GMT - Launch Site: Baikonur. Launch Complex: LC81. Launch Pad: LC81/23. Launch Vehicle: Proton 8K82K / 11S861. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 369-01.
1992 -
1993 - 10:09 GMT - Launch Site: Poker Flat. Launch Vehicle: Black Brant. Model: Black Brant XII. LV Configuration: Black Brant XII NASA 40.04UE. -
Black Brant UCB Alaska '93 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 1,425 km (885 mi).
1993 - 10:34 GMT - Launch Site: Alcantara. Launch Vehicle: VS-40. LV Configuration: VS-40 PT-01. -
VS-40 Test mission Nation: Brazil. Agency: INPE. Apogee: 950 km (590 mi).
1993 - 14:30 GMT - Launch Site: Plesetsk. Launch Complex: LC16. Launch Pad: LC16/2. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
1994 - -
Chinese satellite accident. Nation: China. Spacecraft: FY-2. The first Fen Yung 2 geostationary weather satellite was undergoing final checkout before being mated to its launch vehicle when a fire and explosion erupted, destroying the vehicle, killing one worker and injuring 20 others.
1998 - 02:42 GMT - Launch Site: Vandenberg. Launch Complex: RW30. Launch Pad: L-1011. Launch Vehicle: Pegasus XL. Model: Pegasus XL. LV Configuration: Pegasus XL F21. -
TRACE Nation: USA. Program: Small Explorer. Class: Solar. Spacecraft: TRACE. Manufacturer: NASA Goddard Space Flight Center, Greenbelt. Agency: NASA GSF. Perigee: 602 km (374 mi). Apogee: 652 km (405 mi). Inclination: 97.80 deg. Period: 97.10 min. COSPAR: 1998-020A. USAF Sat Cat: 25280. NASA's third Small Explorer, the Transition Region and Coronal Explorer (TRACE), was successfully launched by an Orbital Pegasus XL. The L-1011 carrier aircraft took off from Vandenberg and dropped the Pegasus over the Pacific Ocean. TRACE, a project led by Lockheed's solar physics group, carried a 30-cm extreme ultraviolet imaging telescope which will study the Sun. The telescope mirrors were made by the Smithsonian Astrophysical Observatory. TRACE had an 8.5 arcmin field of view and 1 arcsecond resolution.
1999 - 11:28 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U. -
Progress M-41 Nation: Russia. Program: Mir. Payload: Progress M s/n 241. Class: Manned. Type: Logistics. Spacecraft: Progress M. Manufacturer: RKK Energiya im. S.P. Korolyov, Kaliningrad-Korolyov. Agency: RKA. Perigee: 336 km (208 mi). Apogee: 361 km (224 mi). Inclination: 51.60 deg. Period: 91.51 min. COSPAR: 1999-015A. USAF Sat Cat: 25664. Duration: 105.99 days. Decay Date: 1999-07-17. Flight: Mir EO-27, Mir EO-26/-27. Resupply craft docked uneventfully with the Mir complex two days later. It also delivered the Sputnik-99 amateur radio satellite, launched into orbit by hand by the cosmonauts during an EVA on April 16. Still hopeful of finding a backer to pay to keep Mir in space, Progress M-41 began a series of engine burns in late April to raise the orbit of the station. It finally undocked from Mir at 11:20 GMT on July 17 and was deorbited over the Pacific later the same day.
1999 - 22:03 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: ELA2. Launch Vehicle: Ariane 42P. Model: Ariane 42P. LV Configuration: Ariane 42P V117.
2000 - 07:34 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Vehicle: Skylark. Model: Skylark 7. LV Configuration: Skylark 7 TEXUS 38. -
Skylark TEXUS 38 Microgravity mission Nation: Sweden. Agency: SSC. Apogee: 250 km (150 mi).
2003 - 01:53 GMT - Launch Site: Plesetsk. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / ML. -
Molniya 1-92 Nation: Russia. Payload: Molniya 1T-26 or 28. Mass: 1,660 kg (3,650 lb). Class: Communications. Type: Military. Spacecraft: Molniya-1T. Manufacturer: NPO Prikladnoy Mekhaniki. Agency: VKS. Perigee: 655 km (406 mi). Apogee: 39,693 km (24,664 mi). Inclination: 62.90 deg. Period: 717.60 min. COSPAR: 2003-011A. USAF Sat Cat: 27707.
Born on this day in:
Died on this day in: . American Manager.
- 1969 - Boris Sergeyevich Stechkin. Russian Engineer.
- 1998 - Eberhard Friedrich Michael Rees. German American Manager.
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