Encyclopedia Astronautica
March 15


March 15 Chronology


1912 March 15 - .
1928 March 15 - . Launch Vehicle: Opel.
  • First rocket car - . Nation: Germany. Related Persons: Valier; Opel. Max Valier campaigned to get automobile magnate Fritz von Opel interested in rocket-powered automobiles. Valier proposed to use different combinations of compressed black powder rockets manufactured by Friedrich Wilhelm Sander of Wesermuende. Sander's rockets were 80 cm long, 12.5 cm in diameter, and could came in two versions. The centre-bore rockets provided 180 kgf for 3 seconds, while the end-burners provided 20 kgf for 30 seconds. Valier proposed to use combinations of these motors to first boost an automobile to high speed with the high-thrust rockets, then use low-thrust units to maintain velocity. This had no practical application but would demonstrate the potential of rockets to the German public, at the same time giving Opel publicity. The first secret test, at Ruesselsheim, used a one high thrust and one low thrust motor in a small stock Opel. The results were unimpressive - the vehicle went only 140 m in 35 seconds.

1932 March 15 - .
  • Birth of Alan LaVerne 'Al' Bean - . Nation: USA. Summary: American test pilot astronaut. Flew on Apollo 12, Skylab 3. Fourth person to walk on the moon..

1933 March 15 - .
1934 March 15 - .
  • Saenger rocket engine - . Nation: Austria. Related Persons: Saenger. Summary: Saenger's Experiment Number 25 is the first to successfully sustain combustion. The water-cooled combustion chamber sustains an internal pressure of 15 atmospheres for 30 seconds..

1944 March 15 - . Launch Site: Peenemuende. LV Family: V-2. Launch Vehicle: V-2.
  • V-2 problems begin to be understood - but Peenemuende Rocket Team leaders arrested by SS - . Nation: Germany. Related Persons: Dornberger; Hitler; Riedel, Walter; Steinhoff, Ernst. The cause of early detonation of the warhead during the engine burn time is understood, but the crashes at the end of the trajectory are still a mystery. Dornberger is ordered to report to Hitler at Berchtesgaden. The call is received at 7 pm in the evening, following a bomb raid and ice storm. Dornberger is told that on the following morning Von Braun, Riedel II, and Groettrup are to be arrested for sabotage of the A4 program. Groettrup selects Dr Steinhoff as his representative. The men are accused of not putting all their energy in development of the A4 as a weapon - instead only using the financing of the Reich to support their private plans for manned spaceflight. Dornberger know he cannot complete the program without these men - Von Braun and Riedel were the key leaders, and Groettrup was head of the electrical systems section. Dornberger finally achieves their release by demonstrating to the SS that the biggest impediment to the program was Hitler's dream that the A4 would never reach London. After a few days in detention, Von Braun was moved to Schwedt, and then freed. The others were allowed out a bit later.

1945 March 15 - . Launch Vehicle: EA 1941. FAILURE: Exploded after 5 seconds..
  • EA 1941 - . Nation: France. Related Persons: Barre. Apogee: 1.00 km (0.60 mi). Summary: Launched from Toulon, France. Intended to take a 25 kg payload to 100 km altitude, the rocket instead veered off course and crashed after 5 seconds of flight..

1946 March 15 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 number 1.
  • V-2 static fired - . Nation: Germany. Related Persons: von Braun. Summary: First American-assembled V-2 static fired at White Sands Proving Ground..

1947 March 15 - .
1950 March 15 - .
  • Tikhonravov wrote a seminal paper on the potential uses of artificial satellites. - . Nation: USSR.

1951 March 15 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Hermes. Launch Vehicle: Hermes A-1. LV Configuration: Hermes A-1 5.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 24 km (14 mi).

1953 March 15 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5. FAILURE: Failure.
  • Phase I state trials launch - . Nation: USSR. Agency: Korolev. Apogee: 0 km ( mi). Unsuccessful. First Phase I trials launch of the 8 remaining rockets of the first production lot were fired, of which 6 reached the target area. The first launch was on 15 March 1953. The first successful flight was on 2 April 1953. The first full range flight came on 19 April 1953.

1955 March 15 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1851T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1956 March 15 - . 00:36 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC6. LV Family: Redstone. Launch Vehicle: Jupiter A. LV Configuration: Jupiter A RS-18. FAILURE: Early cut-off caused by Incorrect guidance cut-off equation pre-setting. ST-80 gyro spilled at 310 sec..
  • Jupiter A - . Nation: USA. Agency: USA. Apogee: 90 km (55 mi). The first Jupiter A launching, by ABMA at Cape Canaveral. RS-18 was launched at 1936 hours EST from AMR. The flight was successful. The scheduled launching date of this missile was 13 March. Three holds were called because of LOX difficulties, telemetry difficulties, and replacement of a gate valve. The actual range was 133.58 nm; 10.3 nm under; and 5.66 nm right of the intended impact point. Separation occurred before the missile gained its correct velocity. Improper assumption of propellant flow for the trajectory calculation was primarily responsible for the incorrect cut-off. The primary test objectives were to test the complete guidance and control system to establish the performance qualities of the complete missile system. Missed aimpoint by 19,100 m.

1960 March 15 - . LV Family: Saturn I. Launch Vehicle: Saturn I.
  • Saturn I transferred to NASA. - . Nation: USA. Related Persons: von Braun. Program: Apollo. The Army Ballistic Missile Agency's Development Operations Division and the Saturn program were transferred to NASA after the expiration of the 60-day limit for congressional action on the President's proposal of January 14. (The President's decision had been made on October 21, 1959.) By Executive Order, the President named the facilities the "George C. Marshall Space Flight Center." Formal transfer took place on July 1.

1960 March 15 - . Launch Site: White Sands. Launch Complex: White Sands LC36. Launch Pad: ALA3?. LV Family: Redstone. Launch Vehicle: Redstone. LV Configuration: Redstone 2014.
  • T-1 Capsule operational test launch - . Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Summary: Successful missile test with T-1 Capsule. Missed aimpoint by 295 m..

1961 March 15 - .
  • Mercury Bermuda tracking station agreement. - . Nation: USA. Program: Mercury. Summary: United States and United Kingdom signed formal agreement covering Mercury tracking stations on Bermuda..

1961 March 15 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2X-10.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1961 March 15 - . 17:47 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.49GT.
  • Cajun fin test - . Nation: USA. Agency: NASA. Apogee: 130 km (80 mi).

1962 March 15 - . LV Family: Atlas. Launch Vehicle: Atlas D.
  • Carpenter replaces Slayton on Mercury-Atlas 7 (MA-7) - . Nation: USA. Program: Mercury. Flight: Mercury MA-7. Summary: NASA Headquarters publicly announced that Scott Carpenter would pilot the Mercury-Atlas 7 (MA-7) manned orbital mission replacing Donald Slayton. The latter, formerly scheduled for the flight, was disqualified because of a minor erratic heart rate..

1963 March 15 - . 11:38 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 46D. FAILURE: Failure. Failed Stage: 1.
  • TALL TREE 1 operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 300 km (180 mi).

1964 March 15 - . 02:44 GMT - . Launch Site: Andoya. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache Ferdinand 7.
  • Ferdinand 7 Ionosphere / plasma mission - . Nation: Norway. Agency: NDRE. Apogee: 134 km (83 mi).

1965 March 15 - .
  • Cosmos 57 lands. - . Nation: USSR. Related Persons: Belyayev; Leonov. Program: Voskhod. Flight: Voskhod 2. Spacecraft: Voskhod; Zenit-4. The Zenit-4 fitted with the airlock attachment ring successfully lands at 12:09, 170 km south of Kustanin (and 50 km north of the aim point). Later procedures for emergency landing on the first, second, and third orbits are discussed. The cosmonauts want to discuss the possibility of their taking action if the airlock fails to jettison (even though there are redundant systems to ensure this). Leonov discuses a method of inflating the airlock, his opening the hatch from the spacecraft, checking all connections, then returning to the capsule and attempting again. Data arrives in the evening from the recovered Zenit - the rotation rates are acceptable, Voskhod-2 is clear to launch on 18 March. In the evening the cosmonauts conduct interviews with journalists.

1965 March 15 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 636. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-21.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1965 March 15 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 636. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-158.
  • Surface launch test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1965 March 15 - . 11:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/15. LV Family: Kosmos 3. Launch Vehicle: Kosmos 65S3. LV Configuration: Kosmos 65S3 04L.
  • Cosmos 61 - . Mass: 50 kg (110 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1. Decay Date: 1968-01-15 . USAF Sat Cat: 1267 . COSPAR: 1965-020A. Apogee: 1,737 km (1,079 mi). Perigee: 262 km (162 mi). Inclination: 56.0000 deg. Period: 105.10 min.
  • Cosmos 63 - . Mass: 50 kg (110 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1. Decay Date: 1967-11-04 . USAF Sat Cat: 1269 . COSPAR: 1965-020C. Apogee: 1,673 km (1,039 mi). Perigee: 259 km (160 mi). Inclination: 56.0000 deg. Period: 104.40 min.
  • Cosmos 62 - . Mass: 50 kg (110 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1. Decay Date: 1968-09-24 . USAF Sat Cat: 1268 . COSPAR: 1965-020B. Apogee: 1,712 km (1,063 mi). Perigee: 259 km (160 mi). Inclination: 56.0000 deg. Period: 104.80 min.

1966 March 15 - .
  • Cosmos 110 landing commission - . Nation: USSR. Program: Voskhod. Flight: Voskhod 3. Spacecraft: Voskhod. The State Commission meets on the 21st day of flight. The life forms are still alive, although the atmosphere in the cabin isgradually worsening (oxygen has gone from 143 to 136 mm Hg and the carbon dioxide level has gone up from 0.89% to 0.91%). The flight duration objective has been fulfilled, and although the designers say the ECS could run for a total of 36 days, it is decided to bring the capsule down within the next two days. A landing commission of 25 military and engineering representatives is formed to oversee the process. It is decided to bring the capsule down on the 330th orbit, on 16 March, with an emergency re-entry possible at 15:30 on 15 March if the cabin parameters worsen.

1967 March 15 - .
  • Plans for recovery of returning manned lunar spacecraft. - . Nation: USSR. Summary: Military-Industrial Commission (VPK) Decree 42 'On search service for returning missions from the Moon' was issued..

1967 March 15 - . LV Family: N1. Launch Vehicle: N1.
  • CIA reports on Soviet space developments - . Nation: USSR. Program: Lunar L3. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-LOK. Summary: CIA reports accurately development of N-1, Almaz, Proton, etc.... even states 100,000 kg large space station in development for launch by N-1 by 1969. CIA does not expect lunar landing until early 1970's..

1968 March 15 - .
  • HL-10 Flight 2 - . Crew: Gentry. Payload: HL-10 flight 2. Nation: USA. Related Persons: Gentry. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: HL-10. Summary: Maximum Speed - 684 kph. Maximum Altitude - 13720 m. Flight Time - 243 sec..

1968 March 15 - . 03:43 GMT - . Launch Site: Kerguelen. LV Family: Belier. Launch Vehicle: Dragon 2B. LV Configuration: Dragon 2B D-251A.
  • FU-171 VLF / Ions Ionosphere mission - . Nation: France. Agency: CNES. Apogee: 400 km (240 mi).

1968 March 15 - . 07:10 GMT - . Launch Site: Fort Churchill. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AE07.290.
  • Auroral P / F Aurora / plasma mission - . Nation: USA. Agency: AFCRL. Apogee: 160 km (90 mi).

1968 March 15 - . 19:04 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.209CS.
  • AS&E Solar x-ray mission - . Nation: USA. Agency: NASA. Apogee: 155 km (96 mi).

1968 March 15 - . 19:11 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.10UI.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 290 km (180 mi).

1969 March 15 - . 05:06 GMT - . Launch Site: Poker Flat. LV Family: Honest John. Launch Vehicle: HJ Nike Hydac. LV Configuration: HJ Nike Hydac SECEDE R6.
  • Far infrared barium release Aeronomy mission - . Nation: USA. Agency: DARPA. Apogee: 165 km (102 mi).

1969 March 15 - . 12:15 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 271 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 8.00 days. Decay Date: 1969-03-23 . USAF Sat Cat: 3807 . COSPAR: 1969-023A. Apogee: 324 km (201 mi). Perigee: 196 km (121 mi). Inclination: 65.4000 deg. Period: 89.70 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1969 March 15 - . 17:55 GMT - . Launch Site: Kiruna. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache K-NA-11.
  • DLR K-NA-11 Aeronomy / ionosphere / Fields mission - . Nation: Germany. Agency: DFVLR. Apogee: 226 km (140 mi).

1969 March 15 - . 20:54 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 2. LV Configuration: Skylark 2 S43/2.
  • ESRO S43 / 2 Aurora mission - . Nation: Europe. Agency: ESRO. Apogee: 211 km (131 mi).

1969 March 15 - . 22:31 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C52/1.
  • ESRO C52 / 1 Aurora mission - . Nation: Europe. Agency: ESRO. Apogee: 136 km (84 mi).

1970 March 15 - .
  • Definition studies for a second Orbital Workshop (Skylab II). - . Nation: USA. Program: Skylab. Flight: Skylab B. Spacecraft: Skylab. Definition studies for a second Orbital Workshop (Skylab II) were under study. Mission objectives would respond to the following major objectives: continued development and expansion of the ability to live, work, and operate effectively in space; exploitation of space for practical benefits through the observation of Earth and its environment; and the use of space for scientific research.

1970 March 15 - . 13:35 GMT - . Launch Site: Andoya. LV Family: Black Brant. Launch Vehicle: Black Brant 4A.
  • DLR A-BB4-28 Eva Ionosphere / plasma mission - . Nation: Germany. Agency: DFVLR. Apogee: 650 km (400 mi).

1971 March 15 - .
  • Major DOS training exercise by third crew. - . Nation: USSR. Related Persons: Dobrovolsky; Volkov; Patsayev; Shatalov; Yeliseyev; Sevastyanov. Program: Salyut. Flight: Soyuz 10; Soyuz 11; Soyuz 12 / DOS 1. Spacecraft: Salyut 1. The third, back-up DOS crew of Dobrovolsky, Volkov and Patsayev train in the DOS trainer. All of the crews have made good runs, with no mistakes or failures. Shatalov, after training on the DOS simulator, now supports Mishin's 30 day flight approach. He has also talked to Yeliseyev and Sevastyanov about the matter. He believes there may be a very different reaction to zero-G from individual to individual, and the Soyuz 9 crew may have been the wrong two individuals.

1971 March 15 - . Launch Site: Baikonur. LV Family: UR-100. Launch Vehicle: UR-100K.
  • Last State trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1971 March 15 - . Launch Site: Hall Beach. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.126GE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1971 March 15 - . Launch Site: Cape Parry. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.122GE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1971 March 15 - . 17:55 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 2. LV Configuration: Skylark 2 S87/1.
  • ESRO S87 / 1 Ionosphere mission - . Nation: Europe. Agency: ESRO. Apogee: 188 km (116 mi).

1971 March 15 - . 18:17 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Apogee: 150 km (90 mi).

1971 March 15 - . 23:00 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 632. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3E-39.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1972 March 15 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle booster decision - . Nation: USA. NASA decided that the shuttle booster will be 2 x 156 inch solid rocket motors. This would reduce the total development cost by $700 million, from $ 5.85 billion to $ 5.15 billion. It was also decided to delete the requirement for the shuttle to be equipped with air-breathing engines for final approach and ferry, and to add Abort Solid Rocket Motors that would pull the shuttle away from the external tank in case of a failure of the solid rocket boosters or external tank during the first portion of the ascent to orbit.

1972 March 15 - . 13:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 478 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4M. Duration: 13.00 days. Decay Date: 1972-03-28 . USAF Sat Cat: 5885 . COSPAR: 1972-015A. Apogee: 282 km (175 mi). Perigee: 176 km (109 mi). Inclination: 65.0000 deg. Period: 89.00 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1972 March 15 - . 16:00 GMT - . Launch Site: San Marco. LV Family: Apache. Launch Vehicle: Nike Apache.
  • ISRC-PO-6 Aeronomy mission - . Nation: Italy. Agency: CRS. Apogee: 185 km (114 mi).

1973 March 15 - .
  • San Juan Capistrano Meteorite Fall - . Nation: USA.

1973 March 15 - .
  • Post-Apollo Lunar Programs Office established - . Nation: USA. Program: Apollo. Flight: Apollo 15. Spacecraft: Apollo ALSEP. A Lunar Programs Office, under which the Lunar Data Analysis and Synthesis Program would be conducted, was established in the Office of Space Science, NASA Hq. The office was responsible for continued operation and collection of data from the Apollo lunar surface experiment packages and the Apollo 15 subsatellite; Apollo surface and orbital science data analysis by principal investigators; development of selenodetic, cartographic, and photographic products; continued lunar laser ranging experiment; continued lunar sample analysis; lunar supporting research and technology; and advanced program studies.

1973 March 15 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: SSBS. Launch Vehicle: SSBS S02. LV Configuration: SSBS S02 2602.
  • S02C 2602 test - . Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1974 March 15 - .
  • Death of Werner Tiller - . Nation: Germany; USA. Related Persons: Tiller. Summary: German engineer in WW2, member of the Rocket Team in the United States thereafter..

1974 March 15 - . 20:00 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere/Chemical release/Plasma mission - . Nation: USSR. Apogee: 173 km (107 mi).

1975 March 15 - . 04:10 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.15UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 214 km (132 mi).

1975 March 15 - . 07:00 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.39UG.
  • JHU UVT F8 (Saturn) Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 261 km (162 mi).

1975 March 15 - . 16:34 GMT - . Launch Site: Thumba. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P70T/C.
  • ISRO-18.17 Ionosphere mission - . Nation: UK. Agency: SRC. Apogee: 147 km (91 mi).

1976 March 15 - .
  • Start functional checkout, Enterprise - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Start functional checkout, Enterprise (OV-101)..

1976 March 15 - . 01:25 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 3C. LV Configuration: Titan IIIC 23C-12 (3C-30).
  • LES 8 - . Mass: 454 kg (1,000 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Communications technology satellite. Spacecraft: LES. Completed Operations Date: 1992-01-01 . USAF Sat Cat: 8746 . COSPAR: 1976-023A. Apogee: 35,835 km (22,266 mi). Perigee: 35,728 km (22,200 mi). Inclination: 11.4000 deg. Period: 1,435.80 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication. Also tested pulsed plasma engines. Positioned in geosynchronous orbit over the Atlantic Ocean at 1976-77; over the Americas at 106-110 deg W in 1978-1986; over the Atlantic Ocean 60-70 deg W in 1987-1991;over the Americas at 94-106 deg W in 1991-1992. As of 6 September 2001 located at 105.16 deg W drifting at 0.010 deg E per day. As of 2007 Mar 9 located at 107.51W drifting at 0.001E degrees per day.
  • Solrad 11B - . Mass: 181 kg (399 lb). Nation: USA. Agency: USAF. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: Solrad. USAF Sat Cat: 8749 . COSPAR: 1976-023D. Apogee: 116,645 km (72,479 mi). Perigee: 115,720 km (71,900 mi). Inclination: 25.6000 deg. Period: 7,116.70 min. Summary: Solar radiation data. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..
  • Solrad 11A - . Mass: 181 kg (399 lb). Nation: USA. Agency: USAF. Class: Astronomy. Type: Solar astronomy satellite. Spacecraft: Solrad. USAF Sat Cat: 8748 . COSPAR: 1976-023C. Apogee: 119,180 km (74,050 mi). Perigee: 118,383 km (73,559 mi). Inclination: 25.7000 deg. Period: 7,344.30 min. Summary: Solar radiation data. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..
  • LES 9 - . Mass: 454 kg (1,000 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Communications technology satellite. Spacecraft: LES. Completed Operations Date: 1992-01-01 . USAF Sat Cat: 8747 . COSPAR: 1976-023B. Apogee: 35,825 km (22,260 mi). Perigee: 35,745 km (22,210 mi). Inclination: 17.0000 deg. Period: 1,436.00 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication. Also tested pulsed plasma engines. Positioned in geosynchronous orbit over the Atlantic Ocean at 30-40 deg W in 1976-78; over the Americas at 90-100 deg W in 1980-81; over the Americas at 100-106 deg W in 1981-1990; over the Atlantic Ocean 10 deg W in 1991; over the Americas at 105 deg W in 1992-on. As of 1 September 2001 located at 103.85 deg W drifting at 0.023 deg W per day. As of 2007 Mar 11 located at 107.07W drifting at 0.018W degrees per day.

1977 March 15 - . 21:06 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1978 March 15 - . 15:57 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53746-315.
  • Cosmos 994 - . Mass: 920 kg (2,020 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Tsiklon. USAF Sat Cat: 10731 . COSPAR: 1978-028A. Apogee: 1,007 km (625 mi). Perigee: 971 km (603 mi). Inclination: 82.9000 deg. Period: 104.90 min. Summary: Military navigation satellite..

1979 March 15 - . 02:58 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47168-312.
  • Cosmos 1081 - . Payload: Strela-1M no. 169. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11296 . COSPAR: 1979-024A. Apogee: 1,465 km (910 mi). Perigee: 1,404 km (872 mi). Inclination: 74.0000 deg. Period: 114.50 min. Summary: Eight satellites launched by a single carrier rocket..
  • Cosmos 1084 - . Payload: Strela-1M no. 172. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11299 . COSPAR: 1979-024D. Apogee: 1,464 km (909 mi). Perigee: 1,462 km (908 mi). Inclination: 74.0000 deg. Period: 115.20 min.
  • Cosmos 1083 - . Payload: Strela-1M no. 171. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11298 . COSPAR: 1979-024C. Apogee: 1,466 km (910 mi). Perigee: 1,443 km (896 mi). Inclination: 74.0000 deg. Period: 115.00 min.
  • Cosmos 1082 - . Payload: Strela-1M no. 170. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11297 . COSPAR: 1979-024B. Apogee: 1,465 km (910 mi). Perigee: 1,423 km (884 mi). Inclination: 74.0000 deg. Period: 114.80 min.
  • Cosmos 1086 - . Payload: Strela-1M no. 174. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11301 . COSPAR: 1979-024F. Apogee: 1,482 km (920 mi). Perigee: 1,466 km (910 mi). Inclination: 74.0000 deg. Period: 115.40 min.
  • Cosmos 1085 - . Payload: Strela-1M no. 173. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11300 . COSPAR: 1979-024E. Apogee: 1,504 km (934 mi). Perigee: 1,465 km (910 mi). Inclination: 74.0000 deg. Period: 115.70 min.
  • Cosmos 1088 - . Payload: Strela-1M no. 176. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11303 . COSPAR: 1979-024H. Apogee: 1,548 km (961 mi). Perigee: 1,465 km (910 mi). Inclination: 74.0000 deg. Period: 116.10 min.
  • Cosmos 1087 - . Payload: Strela-1M no. 175. Mass: 40 kg (88 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1M. USAF Sat Cat: 11302 . COSPAR: 1979-024G. Apogee: 1,524 km (946 mi). Perigee: 1,465 km (910 mi). Inclination: 74.0000 deg. Period: 115.90 min.

1979 March 15 - . 05:20 GMT - . Launch Site: White Sands. LV Family: Astrobee. Launch Vehicle: Astrobee F. LV Configuration: Astrobee F NASA 25.45UH.
  • X-ray astronomy mission - . Nation: USA. Agency: NASA. Apogee: 216 km (134 mi).

1980 March 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ABRV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 March 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TDV-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1982 March 15 - . 04:39 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 305-02.
  • Gorizont 5 - . Payload: Gorizont s/n 14L. Mass: 2,100 kg (4,600 lb). Nation: USSR. Agency: MOM. Class: Communications. Type: Civilian communications satellite. Spacecraft: Gorizont . Completed Operations Date: 1989-11-24 . USAF Sat Cat: 13092 . COSPAR: 1982-020A. Apogee: 36,427 km (22,634 mi). Perigee: 36,139 km (22,455 mi). Inclination: 9.7000 deg. Period: 1,461.50 min. Stationed at 53 deg E. Provision of telephone and telegraph radiocommunications and transmission of television programmes. Positioned in geosynchronous orbit at 53 deg E in 1982-1986; 96 deg E in 1986-1989 As of 28 August 2001 located at 156.27 deg E drifting at 6.267 deg W per day. As of 2007 Mar 10 located at 91.82E drifting at 6.281W degrees per day.

1982 March 15 - . 06:38 GMT - . Launch Site: Poker Flat. LV Family: Tomahawk Sandia. Launch Vehicle: Taurus Tomahawk. LV Configuration: Taurus Tomahawk NASA 34.08UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).

1983 March 15 - . 02:33 GMT - . Launch Site: Punta Lobos. LV Family: Terrier. Launch Vehicle: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.19UE.
  • CONDOR Plasma mission - . Nation: USA. Agency: NASA. Apogee: 520 km (320 mi).

1983 March 15 - . 22:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: Kosmos 3. Launch Vehicle: K65M-RB.
  • Cosmos 1445 - . Mass: 1,000 kg (2,200 lb). Nation: USSR. Agency: MO. Program: Buran. Class: Manned. Type: Manned spaceplane. Spacecraft: BOR-4. Duration: 0.0700 days. Decay Date: 1983-03-16 . USAF Sat Cat: 13883 . COSPAR: 1983-017A. Apogee: 208 km (129 mi). Perigee: 158 km (98 mi). Inclination: 50.7000 deg. Period: 88.20 min. Summary: Subscale Spiral spaceplane. After 1.25 revolutions of the earth, deorbited and recovered by Soviet naval forces in the Indian Ocean, 556 km south of the Cocos Islands ..

1984 March 15 - . 17:05 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32. Launch Pad: LC32/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1544 - . Payload: Tselina-D no. 45. Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. USAF Sat Cat: 14819 . COSPAR: 1984-027A. Apogee: 618 km (384 mi). Perigee: 591 km (367 mi). Inclination: 82.5000 deg. Period: 96.80 min.

1985 March 15 - . LV Family: Energia. Launch Vehicle: Energia.
  • Energia cold flow tests. - . Nation: USSR. Program: Buran. Spacecraft: Buran. From March-October 1985 the Ts core stage was back on the UKSS test/launch stand for cold flow tests. A total of nine cryogenic fuelling cycle were completed with the 4M Energia mock-up, representing the first operational use in the world of super-chilled hydrogen.

1985 March 15 - . 02:05 GMT - . Launch Site: Sonde Stromfjord. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX GL A21.426.
  • PIIE Plasma mission - . Nation: USA. Agency: USAF GL. Apogee: 429 km (266 mi).

1985 March 15 - . 17:37 GMT - . Launch Site: Fort Churchill. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.50UU.
  • CWAS 9 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 75 km (46 mi).

1986 March 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT114GM Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1986 March 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT113GM-1 Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1987 March 15 - . 20:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 88 km (54 mi).

1988 March 15 - . 18:50 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32. Launch Pad: LC32/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1933 - . Payload: Tselina-D no. 65. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. USAF Sat Cat: 18958 . COSPAR: 1988-020A. Apogee: 629 km (390 mi). Perigee: 605 km (375 mi). Inclination: 82.5000 deg. Period: 97.10 min.

1989 March 15 - . 15:45 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 79 km (49 mi).

1990 March 15 - . 19:21 GMT - . Launch Site: Biscarosse. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A Sphere.
  • DYANA DBS41 Aeronomy mission - . Nation: USA. Agency: DGA. Apogee: 90 km (55 mi).

1992 March 15 - . 22:46 GMT - . Launch Site: White Sands. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.82UU.
  • CWAS 22 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1993 March 15 - .
  • Mir News 165: Mir-DAILY ROUTINE - . Nation: Russia. Program: Mir. Flight: Mir EO-13. After the docking of freighter Progress-M16 the crew continued their reparation and replacement work on the systems of the complex. They did not much experimental work apart from geophysical observations. They needed all their working time for technical maintenance. They repaired a number of gyrodynes and Manakov was positive about the results of that 'high priority' work. I hope that I was right for Manakov is a great optimist. The VDU (the external movements control motor in the Sofora- girder) is still unserviceable due to software problems. Of great concern for crew and experts remain the complicated systems to maintain the climate in that what is like an 'iron lung'. In contradiction to the 'iron lungs' for medical use this one has to feed and regenerate itself. Wear of parts of that complicated complex results in malfunctioning, so the crew repeatedly gets warnings about hitches, but also by more noise than originally had been foreseen. Daily they speak about the BKV-3, a system to restore the condition of the air. When the crew gets permission to switch that system off (getting the command G-24), they enjoy the silence. Polishchuk did a lot of repair work on that BKV-3.

    EXTRA VEHICULAR ACTIVITIES (EVA-S):

    Shortly we can hear the crew speak about preparations for a series of 4 EVA-s. For the 1st one the 16th of April has been mentioned. During the first 3 EVA-s the cosmonauts will have to replace the solar panels from the Kristall module to the Kvant-1. The 4th one is for the removal of materials which for a long time had been exposed to the influences of open space. The solar panels have to be replaced to make future operations possible. To execute the planned docking operations of Buran and Space Shuttle to that Kristall module it has to be redocked to the forward axial (PKhO) docking port. A second reason to replace those solar panels is the fact that some solar panels hinder other ones. Daily the crew has to economise the power consumption of the complex. Polishchuk is responsible for that and in Manakov's opinion he is an expert in that field.

    MODULES:

    Possibly the plans for the launch of the Modules Priroda and Spektr have been altered. The first Module to be launched for a docking with Mir should be a technological one. So Priroda is 2d on schedule. This is a pity for Priroda is ready for launch.

    RETURN CAPSULES: Progress-M16 does not carry such a capsule and the use of such a container from Progress-M17 has not been planned. The return capsules are for 100% reliable, but due to the little amount of freight to be brought back, return capsule operations are too expensive.

    Chris van den Berg, NL-9165/A-UK3202.


1994 March 15 - .
  • Mir News 209: Launch Progress-M22 postponed - . Nation: Russia. Program: Mir. Flight: Mir EO-15; Mir LD-4. This freighter was on schedule to be launched on 16 or 18.03. Due to very bad weather conditions (blizzards) the launch has been put back for a while. Possibly the exact date of launch will be published on 17.03.94.

    Fire on Baykonur: On 7.03.94 a heavy fire broke out in a MIK (Assembly and test complex) and spread to a Maintenance Unit Headquarters. There the fire damaged a Telemetry installation. The fire caused a damage of appr. 1.7 a 1.8 million dollars. The Russians declared that space-programs will not suffer from this event.

    Progress-M17: This freighter has been flying autonomously from 11.08.93 for a duration test of its systems. The Russians planned to leave the Progress-M17 in orbit for a year and a half on request by the Americans who want to use modified versions of the Soyuz-TM-ships for ACRV (assured crew return vehicle) for the space station Alpha. A test flight with a Progress-M was useful for a lot of systems of this freighter are the same as those of the Soyuz-TM. During an orbit manoeuvre in December 1993 something went wrong and the Progress-M17 came in a very low perigee from where it decayed naturally by burning up in the Earth's atmosphere on 3.03.94 at 0406 UTC

    Tracking ships: The tracking ship Cosmonaut Pavel Belyayev is floating somewhere in the Atlantic for the support of spaceflight operations which have nothing to do with the Mir-station. Nevertheless the ship now and then assists TsUP for communications with the Mir-station. This took place on 13.03- .94 at 2004 UTC and on 14.03.94 at 2045 UTC, so out of our range. We can expect that within due time we can hear Mir- radio traffic relayed by the KPB or one of the other ships.

    Chris v.d. Berg, NL-9165/A-UK3202


1995 March 15 - . 20:21 GMT - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.106NP.
1996 March 15 - . Launch Site: White Sands. LV Family: DC-X. Launch Vehicle: DC-X. LV Configuration: DC-XA.
  • DC-XA Rollout - . Nation: USA.

1996 March 15 - . 01:04 GMT - .
1998 March 15 - .
  • Mir News 412: Progress-M38 - . Nation: Russia. Program: Mir. Flight: Mir NASA-6; Mir EO-25. The launch of this freighter from Baykonur took place on 14.03.1998 at 22.45.55 UTC (for Moscow already 15.03.1998 01.45.55 DMV -Moscow Decree Time). During the pass in the 3rd orbit I monitored the Telemetry transmitters of this ship between 0321-0324 UTC. During the pass in the 4th orbit the Telemetry transmitters (166 and 165 mc) and the beacon on 922.755mc could be heard between 0450 and 0458 UTC. TCA for me was at 0453 UTC.

    The most important cargo is the VDU. This is the external thruster which has to be installed in the Sofora mast on Kvant-1 during one of the EVA's in the future. The new VDU will replace the old one which almost run out of fuel. Under the cargo is a new lock for the EVA hatch of Module-D, the necessary tools for the repair of that hatch and of course the normal cargo: food, post and some other convenient items for the crew. Progress-M38 has to dock at the Kvant-1 aft docking port (+X-axis) on 17.03.1998 at about 0027 UTC. In principle approach and docking will be executed in the automatic mode with the system Kurs.

    Progress-M37:

    Today (15.03) Progress-M37 will separate from Mir to be put on a destruction course for burning up in the atmosphere over a designated area East of New-Zealand.

    Mir-routine:

    Last week the cosmonauts worked on the installation of the new BKV-3, the a.c. From 10.03 the BKV-3 is regularly operational and this resulted in decreasing of the almost unbearable high temperatures in the Base Block. The temperature of approx. 35 dgs C. decreased to 28 dgs C. The good functioning of the a.c. makes it possible to use this installation for the filtering of the surplus of condensation secreted by the Vozdukh CO2 scrubber. Thus this condensation can be used for water regeneration purposes and has no longer to be blown into open space.

    To make this possible the Vozdukh in the Base Block had to be modified by a so called 'dehumidifier'. This device is now installed in the neighbourhood of the Vozdukh but it was difficult to find a place for it. Meanwhile something went wrong with he thermal control in the module Priroda, which had a negative effect on some experiments of Andy. After the repair or replacement of a pump the temperatures in Priroda could be controlled again.

    The work was far from easy and they could not always find the necessary parts and equipment for the mounting. This often debauched into discussions with experts on earth. Musabayev normally being in a good mood now and then got upset. He stated that already from the first week the burden of work was too high. There was a great difference between planning and the reality of time schedules for their work in space. On 4.03.1998 he stated that this was the first day they got enough sleep. He emphasised that if you force the crew too much there will be a risk of fatal mistakes. (And indeed during this mission a number of mistakes have been reported. )

    Not only the Russians, but also Andy Thomas complained about matters he did not appreciate. He had no problems with his direct 'leads', but with some organisations. Regularly Andy repeated his complaint that he did not receive his personal E-mails. Last week this resulted in the despatch of a stream E-mails, reaching him by uplink Packet Radio transmissions, also via Altair-2.

    Andy reported problems with the American experiment COCULT. The flow of liquids to feed cells of this experiment was full of air-bubbles. He tried to solve this problem but did not succeed. In conversations with his consultative group he emphasised that he does all what is possible to fulfil the American experimental program, but that he attaches great value to the execution of his physical exercises.

    The forthcoming launch of Progress-M38 and the departure on 15.03.1998 of the old Progress-M37 were mentioned now and then. The crew tried to load as much as possible waste and equipment which was no longer needed in the Progress-M37. Musabayev reported that it was not possible to load the old BKV-3 in that freighter. He gave a higher priority to the dismissal of waste containers, lots of old rags, biological- and domestic garbage.

    More or less the lot of work on the life support systems superseded the attention for the forthcoming departure of the Progress-M38. Only yesterday (14.03) they spoke about the TORU (remote controlled steering of Progress-M from inside Mir), which has to be operational in case the automatic system Kurs should fail.

    On 9.03.1998 a planned communication session of Mir with TsUP via Altair-2 did not take place. Something went wrong with the uplink from Russia to Altair-2. Musabayev who was calling continuously was almost desperate. He needed an urgent advice about immunisation. For me it was interesting to hear how a cosmonaut feels when he thinks that he has been abandoned by earth. During the first communication session via VHF he said that they almost 'suffered an infarct'.

    .

    Chris v.d. Berg, NL-9165/A-UK3202.


1999 March 15 - . 03:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U/Ikar - ST02.
  • Globalstar M022 - . Mass: 222 kg (489 lb). Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25649 . COSPAR: 1999-012A. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min. In the second Soyuz/Ikar launch four Globalstar satellites were delivered with the Ikar upper stage into a 235 km x 899 km x 52.0 degree transfer orbit. The Ikar stage then placed itself and its payload into a 897 km x 950 km x 52.0 degree deployment orbit. Satellite M022 was separated first from the top of the dispenser, followed by ejection of the other three satellites from the sides at 06:37 GMT. After dispensing the satellites, the Ikar deorbited itself on March 16.
  • Globalstar M041 - . Mass: 222 kg (489 lb). Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25650 . COSPAR: 1999-012B. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.
  • Globalstar M046 - . Mass: 222 kg (489 lb). Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25651 . COSPAR: 1999-012C. Apogee: 1,595 km (991 mi). Perigee: 1,594 km (990 mi). Inclination: 52.0000 deg. Period: 118.10 min.
  • Globalstar M037 - . Mass: 222 kg (489 lb). Nation: USA. Agency: Globalstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Globalstar. USAF Sat Cat: 25652 . COSPAR: 1999-012D. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.0000 deg. Period: 114.10 min.

1999 March 15 - . 09:52 GMT - . Launch Site: Alcantara. LV Family: Sonda. Launch Vehicle: VS-30. LV Configuration: VS-30 XV-04.
  • Operacao San Marcos Microgravity mission - . Nation: Brazil. Agency: AEB. Apogee: 128 km (79 mi).

2000 March 15 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
  • Atmospheric Waves Aeronomy mission - . Nation: India. Agency: ISRO. Apogee: 70 km (43 mi).

2001 March 15 - .
2002 March 15 - .
  • ISS Status Report: ISS 02-14 - . Nation: USA. Related Persons: Bursch; Jett; Onufrienko; Walz. Program: ISS. Flight: ISS EO-4. Summary: Expedition Four Commander Yury Onufrienko and Flight Engineers Dan Bursch and Carl Walz aboard the International Space Station continued science experiments and prepared for two spacecraft that will soon visit the outpost.. Additional Details: ISS Status Report: ISS 02-14.

2003 March 15 - .
  • Black Armadillo subscale hover tests. - . Nation: USA. Program: X-Prize. Spacecraft: Black Armadillo. Summary: Armadillo Aerospace (Mesquite, Texas, USA) performed suspended hover tests of their sub-scale (two foot diameter) vehicle. Problems with electronic components and flight control software caused early termination of the tests..

2004 March 15 - .
  • Death of William H Pickering - . Nation: USA. Related Persons: Pickering. Summary: New Zealand-American Chief Designer, Director JPL, 1954-1976. Under his leadership the first successful probes to earth orbit, the Moon, Venus, and Mars were designed, built, and flown (Explorer, Pioneer, Ranger, Mariner,Surveryor, Viking)..

2004 March 15 - . 23:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton-M/Briz-M 535-03.
  • W3A - . Payload: Eurostar 3000S. Mass: 4,250 kg (9,360 lb). Nation: Europe. Agency: Eutelsat. Manufacturer: EADS Astrium. Program: Eutelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 28187 . COSPAR: 2004-008A. Apogee: 35,811 km (22,251 mi). Perigee: 35,761 km (22,220 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Moved from Ariane 5. The satellite was to provide a full range of telecommunications applications including digital DVB broadcasting, multimedia, broadband access and pay-per-use bandwidth for corporate networks over a large zone covering Europe and Africa, for a minimum of 12 years. As of 2007 Mar 10 located at 6.95E drifting at 0.006W degrees per day.

2005 March 15 - . 07:45 GMT - . Launch Site: Poker Flat. Launch Complex: Poker Flat LC2. LV Family: Hawk. Launch Vehicle: Improved Orion. LV Configuration: Improved Orion NASA 30.59UE.
  • DUST Aeronomy / dust mission - . Nation: USA. Agency: NASA. Apogee: 105 km (65 mi).

2008 March 15 - .
  • EVA STS-123-2 - . Crew: Linnehan; Foreman. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.30 days. Nation: USA. Related Persons: Linnehan; Foreman. Program: ISS. Flight: STS-123; ISS EO-16. Summary: The crew continued assembly of the Dextre robotic manipulator, located in a Spacelab pallet attached to the Station truss..

2008 March 15 - .
  • Death of George David Low at Reston, Virginia. Cancer. - . Nation: USA. Related Persons: Low. Summary: American engineer mission specialist astronaut. Flew on STS-32, STS-43, STS-57. Son of former NASA administrator George M Low..

2008 March 15 - . 06:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. Launch Pad: SLC17A. LV Family: Delta. Launch Vehicle: Delta 7925.
  • USA 201 - . Payload: GPS 2R-19M / Navstar 62 / SVN 48. Nation: USA. Agency: Martin. Class: Navigation. Type: Navigation satellite. Spacecraft: GPS Block 2R. USAF Sat Cat: 32711 . COSPAR: 2008-012A. Apogee: 20,223 km (12,565 mi). Perigee: 20,142 km (12,515 mi). Inclination: 55.1000 deg. Period: 718.00 min. The Delta's second stage first cutoff at 06:20 GMT put the stage and payload into a 174 km x 205 km parking orbit. The stage fired again to place the satellite into a 188 km x 20325 km x 40.0 deg transfer orbit. USA 201 fired its apogee motor at 09:21 GMT on 17 March in and placed itself into its operational final orbit.

2009 March 15 - . 23:43 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle.
  • STS-119 - . Call Sign: Discovery. Crew: Archambault; Antonelli; Phillips; Swanson; Acaba; Arnold, Ricky. Payload: Discovery F35 /. Mass: 120,860 kg (266,450 lb). Nation: USA. Agency: NASA. Program: ISS. Class: Manned. Type: Manned spaceplane. Flight: STS-119. Spacecraft: Discovery. Duration: 12.81 days. Decay Date: 2009-03-28 . USAF Sat Cat: 34541 . COSPAR: 2009-012A. Apogee: 353 km (219 mi). Perigee: 335 km (208 mi). Inclination: 51.6000 deg. Period: 91.40 min. Summary: Crew: Archambault, Antonelli, Phillips, Swanson, Acaba, Arnold. ISS assembly mission. Delivered to the ISS and installed the fourth starboard truss segment (ITS S6) and fourth set of solar arrays and batteries..

2011 March 15 - . LV Family: Shahab. Launch Vehicle: Safir-2. LV Configuration: Kavoshgar.
  • Kavoshgar-4 - . Nation: Iran. Apogee: 120 km (70 mi). Summary: R&D launch.

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