See also Born on this Day On this day in: 1947 - Launch Site: Hammaguira. Launch Complex: -. Launch Pad: -.
1947 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: HVAR. Model: HVAR FFAR. -
RM-10 model test flight Nation: USA. Agency: NACA. Apogee: 5.00 km (3.10 mi).
1952 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Corporal. Model: Corporal. LV Configuration: Corporal 17R. -
Test mission Nation: USA. Agency: USA?. Apogee: 30 km (18 mi).
1953 - 10:19 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee XASR-SC-2. LV Configuration: Aerobee XASR-SC-2 SC 28.
1954 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-1. Model: R-1 8A11. LV Configuration: R-1 8A11 No 1910. -
Operational test Nation: USSR. Agency: NII-88. Apogee: 100 km (60 mi).
1957 - Launch Vehicle: X-17.
1958 -
1958 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. -
Beacon Test 1 Balloon test Nation: USA. Agency: NACA LaRC. Apogee: 122 km (75 mi).
1958 - 00:10 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Able. LV Configuration: Thor Able 116. FAILURE: Thor turbopump gearbox failed T+150 sec.
1959 - -
All three military services studying a base on the moon Nation: USA. Spacecraft: Lunex Lunar Expedition, Horizon Lunar Outpost, Navy SLV. Testifying before the Senate Committee on Aeronautical and Space Sciences, Maj. Gen. Bernard A. Schriever, Commander of the Air Force Ballistic Missile Division, stated that all three military services should be studying the possibility of a base on the moon. Up to that point, he felt, all such studies had been "in the blue thinking."
1961 - Launch Vehicle: Kosmos 3. Model: R-14.
1961 - 02:53 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 101. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 58 km (36 mi).
1962 - Launch Vehicle: Nova. Model: Nova 8L.
1962 - -
Indecision on the lunar mission mode causing delays in Apollo program Nation: USA. Program: Apollo. Spacecraft: Apollo LM, Apollo Lunar Landing. MSC Associate Director Walter C. William reported to the Manned Space Flight Management Council that the lack of a decision on the lunar mission mode was causing delays in various areas of the Apollo spacecraft program, especially the requirements for the portions of the spacecraft being furnished by NAA.
1962 - Launch Vehicle: Proton. Model: Proton 8K82. -
Approval to proceed with the UR-500 (8K82) was provided in a Central Committee decree Nation: USSR. Spacecraft: LK-1. Council of Soviet Ministers (SM) Decree 'On start of work on the UR-500 missile and carrier-rocket' was issued. The rocket was to be built initially for the GR-2 requirement - a heavy rocket that could be used to launch large military payloads into space as well as act as a ballistic missile for multiple nuclear warheads up to 100 MT in yield. The decree ordered development of this powerful new rocket to be completed within three years. This was a difficult task, considering the factory and launch facilities that would have to be built to allow testing of the rocket to begin. The draft project UR-500 was completed in 1963.
1962 - 04:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. LV Configuration: Kosmos 63S1 4LK.
1963 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. -
Test mission Nation: USA. Agency: USA. Apogee: 200 km (120 mi).
1963 - 20:59 GMT - Launch Site: Vandenberg. Launch Complex: OSTF1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 65E.
1964 - -
Deletion of the Apollo LEM's front docking capability Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Representatives from a number of elements within MSC (including systems and structural engineers, advanced systems and rendezvous experts, and two astronauts, Edward H. White II and Elliot M. See, Jr.) discussed the idea of deleting the LEM's front docking capability (an idea spawned by the recent TM-1 mockup review). Rather than nose-to-nose docking, the LEM crew might be able to perform the rendezvous and docking maneuver, docking at the spacecraft's upper (transfer) hatch, by using a window above the LEM commander's head to enable him to see his target.
- Additional details.
1964 -
1964 - -
Voskhod plans Nation: USSR. Program: Voskhod, Vostok. Spacecraft: Voskhod, Berkut. Flight: Voskhod 1, Voskhod 2, Vostok 7, Vostok 8, Vostok 9, Vostok 10. Kamanin receives the directive issued by Biryuzov to implement the Voskhod Party resolutions. Four spacecraft will be completed, two in a three-man configuration, to be flown in the second half of 1964, and two in a configuration that will provide an airlock and allow one cosmonaut to exit into open space. Less than a year is allowed to develop the new spacecraft version for the spacewalk, as well as develop the space suit. This will be a crash priority program, and allow Korolev no resources to complete and launch five Vostok spacecraft on manned and life sciences missions beginning in May.
1964 - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 444. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1967 - 15:20 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.117GS. -
OSO-3 calibration Solar x-ray / extreme ultraviolet mission Nation: USA. Agency: NASA. Apogee: 181 km (112 mi).
1967 - -
Crash of Soyuz 1. Cosmonaut Vladimir Mikhailovich Komarov is killed at age 40. Nation: USSR. Program: Soyuz. Flight: Soyuz 1. The decision was made to bring Komarov back due to an undeployed solar panel which reduced electrical power and blocked orientation sensors. Re-entry was successful and the drag chute deployed. However due to a flaw during manufacture, the parachute compartment housing was too rough and the main parachute would not deploy. Komarov released the reserve chute, but it became tangled with the drag chute. The descent module crashed into a field near Orenburg at 03:24 GMT.
- Additional details.
1968 - 03:05 GMT - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 892. -
ST Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1968 - 15:44 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.260IG. -
ISRO 40.02 X-ray astronomy mission Nation: India. Agency: ISRO. Apogee: 159 km (98 mi).
1968 - 16:00 GMT - Launch Site: Baikonur. Launch Complex: LC90/20. Launch Pad: -. Launch Vehicle: Tsiklon. Model: Tsiklon-2A.
1970 - Launch Vehicle: CZ-1.
1970 - Launch Site: Johnston Island. Launch Complex: LE2. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2J. LV Configuration: Thor DSV-2J 225. FAILURE: Failure.
1970 - 00:52 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AMD-VB-25. -
Aurora / ionosphere mission Aurora / ionosphere mission Nation: Canada. Agency: NRCC. Apogee: 288 km (178 mi).
1970 - 07:30 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12. -
Ionosphere mission Nation: USSR. Apogee: 175 km (108 mi).
1970 - 08:53 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.30. -
Ae170? X-ray astronomy mission Nation: USA. Agency: KPNO. Apogee: 274 km (170 mi).
1970 - 13:35 GMT - Launch Site: Jiuquan. Launch Complex: LA2A. Launch Pad: -. Launch Vehicle: CZ-1. Model: CZ-1. -
DFH Mao 1 Nation: China. Payload: DFH 1. Mass: 173 kg (381 lb). Class: Technology. Spacecraft: DFH-1. Agency: MAI. Perigee: 434 km (269 mi). Apogee: 2,162 km (1,343 mi). Inclination: 68.40 deg. Period: 111.60 min. COSPAR: 1970-034A. USAF Sat Cat: 4382. The final campaign to launch China's first satellite began on April 1, 1970, when two DFH-1 satellites and the CZ-1 rocket arrived by train at the Jiuquan Satellite Launch Centre. This was over a year after the first attempt in 1969. Ren Xinmin was project leader and Qi Faren was leader of the DFH-1 experiment team. On April 2 Premier Zhou Enlai called a special meeting in the Great Hall of the People in Beijing for a final readiness review of the satellite and the launch vehicle. Zhou wanted special guarantees that the satellite would transmit the march 'The East is Red' from orbit.
On the morning of April 24, 1970, the first and second stages of CZ-1 were loaded with propellant and stacked. The satellite was mated to the spin-stabilized solid-propellant third stage, and the launcher entered the final eight hours of launch preparation. Weather forecast for the launch at 9:30 p.m. called for clouds at above 7,000 meters and a wind speed of less than 4 to 5 meters per second.
The historic launch came at 9:35 p.m. local time (13:35 UTC). Upon hearing the command "ignition", a launch controller pressed the button to start the rocket engines. The three-stage CZ-1, which was 29.46 meters tall and had a maximum diameter of 2.25 meters, lifted off the launch pad with a thrust of 104 tonnes. Liftoff weight of the CZ-1 was 81.5 tonnes. Rocket expert Shen Jianan recounted that "..as soon as I saw the liftoff on the TV screen inside the bunker, I ran outside. I could only see the beautiful rocket lighting up the night sky and streaking towards the southeast. I ran back inside to listen to the transmissions. Broadcasting on the speaker were status reports like 'capturing target', 'nominal tracking', 'nominal flight', 'nominal second and third stage separation'..." Thirteen minutes after launch, at 9:48 p.m., mission control announced "...satellite and rocket stage separation, satellite enters orbit...the bunker was filled with cheers".
China became the fifth nation after the former Soviet Union, the United States, France and Japan to achieve an indigenous space launch capability. At 9:50 p.m., the National Broadcasting Bureau announced the acquisition of the tune 'East is Red' from the satellite loud and clear. In the following days, the People's Central Broadcasting radio and newspapers in Beijing announced and printed worldwide times of DFH-1 and CZ-1 third stage passages, and directions of travel in the sky. Senior officials in Beijing dispatched a chartered plane to JSLC to bring back Qi and other scientists. In the International Labour Day celebration on May 1, Chairman Mao and Premier Zhou warmly welcomed them at the Tiananmen Square.
1970 - 22:24 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/4. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1971 - -
Landing of Soyuz 10 Nation: USSR. Program: Salyut. Spacecraft: Soyuz 7KT-OK. Flight: Soyuz 10. Only a night landing on Soviet territory was possible, which meant the spacecraft could not be oriented for retrofire. The landing commission started planning for an emergency landing in South America, Africa, or Australia. But Shatalov reported the gyroscopes and orientation sensors were functioning well. He proposed that he orient on the dayside, spin up the gyro platform, and let the gyros orient the spacecraft on the nightside for retrofire. The plan is followed and the spacecraft was targeted for a landing area 80-100 km southwest of Karaganda. PVO radars pick up the capsule as it soars over the Caspian Sea, and a Mi-4 helicopter sights the parachute even before it thumps down, upright, on the steppes. During the landing, the Soyuz air supply became toxic, and Rukavishnikov was overcome and became unconscious. Nevertheless the crew safely landed at 23:40 GMT, 120 km NW of Karaganda. At the cosmodrome, Chertok is assigned to head a special commission to find the cause of the docking failure and correct it before the next mission can be launched. The VVS aircraft leaves at 07:00 for Moscow. Mishin was to accompany the VPK on their aircraft back, but he is drunk and has to go separately at 15:00. The Soyuz 10 crew reaches Chkalovsky Air Base at 14:00 on 26 April and proceed to Star City for further debriefings. Film and photos indicated that the docking system on the Salyut was not damaged, setting the stage for the Soyuz 11 mission.
1971 - 07:32 GMT - Launch Site: San Marco. Launch Complex: -. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B. LV Configuration: Scout B S173C.
1971 - 11:15 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1971 - 23:35 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P54K. -
E field Ionosphere mission Nation: UK. Agency: SRC. Apogee: 162 km (100 mi).
1972 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1972 - 20:57 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.15CS. -
Solar x-ray mission Nation: USA. Agency: NASA. Apogee: 203 km (126 mi).
1974 - 11:50 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
1974 - 13:00 GMT - Launch Site: Sriharikota. Launch Complex: -. Launch Pad: -. Launch Vehicle: RH. Model: RH-560. -
First test Nation: India. Agency: ISRO. Apogee: 280 km (170 mi).
1975 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
FOT-10? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1975 - Launch Site: Baikonur. Launch Complex: LC106. Launch Pad: -. Launch Vehicle: R-36M. -
Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1975 - 08:05 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
1978 - -
Start precombined systems test, Columbia (OV-102) Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Columbia.
1978 - 09:35 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
OT-33 Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1978 - 09:35 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
OT-33 Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1978 - 09:36 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
OT-33 Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1978 - 09:36 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
OT-33 Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1981 - 21:32 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 34B. LV Configuration: Titan 34B 34B-8 (3B-60) / Ascent Agena D. -
Jumpseat 6 Nation: USA. Mass: 700 kg (1,540 lb). Class: Sigint. Spacecraft: Jumpseat. Agency: NRO/USAF. Perigee: 188 km (116 mi). Apogee: 708 km (439 mi). Inclination: 62.70 deg. Period: 93.00 min. COSPAR: 1981-038A. USAF Sat Cat: 12418. SDS 4 not deployed.
1982 - 17:52 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4. -
DASO-12 demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1987 - 12:42 GMT - Launch Site: Baikonur. Launch Complex: LC200/40. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 335-01. FAILURE: Block DM-2 failure, remained in LEO.
1987 - 16:59 GMT - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1990 - 12:33 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39B. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-31R. -
STS-31 Nation: USA. Program: STS. Payload: Discovery F10 / Hubble Space Telescope. Mass: 13,005 kg (28,671 lb). Class: Manned. Type: Spaceplane. Spacecraft: Discovery. Agency: NASA JSC. Perigee: 585 km (363 mi). Apogee: 615 km (382 mi). Inclination: 28.50 deg. Period: 96.70 min. COSPAR: 1990-037A. USAF Sat Cat: 20579. Duration: 5.05 days. Decay Date: 1990-04-29. Crew: Bolden, Hawley, McCandless, Shriver, Sullivan. Flight: STS-31. Deployed HST (Hubble Space Telescope). Payloads: Deployment of Hubble Space Telescope, IMAX camera in payload bay and in crew compartment, Protein Crystal Growth III-03, Investigation Into Polymer Membrane Process-ing- 01, Air Force Maui Optical Site-05, Radiation Monitoring Equipment III-01, Student Experiment 82-16, and Ascent Particle Monitor 01.
1991 - 01:37 GMT - Launch Site: Plesetsk. Launch Complex: LC32. Launch Pad: LC32/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-3.
1995 - Launch Site: White Sands. Launch Complex: LC32. Launch Pad: -. Launch Vehicle: Hera. LV Configuration: Hera 1. -
BRV/Propulsion Test Target mission Nation: USA. Agency: USA. Apogee: 275 km (170 mi).
1996 - 12:27 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7920-10. LV Configuration: Delta 7920-10 D235.
1996 - 13:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M.
1996 - 23:37 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 401A/Centaur. LV Configuration: Titan 401A/Centaur K-16/TC-15 (45E-4).
1997 - -
Senate, 7426, approves chemical-weapons treaty Nation: USA.
1998 -
1998 - 22:38 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7420-10C. LV Configuration: Delta 7420-10C D256.
2001 - 12:32 GMT - -
EVA STS-100-2 Nation: USA. Program: ISS. Class: Manned. Type: Spaceplane. Crew: Hadfield, Parazynski. Flight: STS-100. EVA Duration: 0.32 days. The astronauts removed a temporary communications antenna from Unity, and connected up power to the Canadarm-2. Susan Helms aboard Destiny then used the arm's LEE A manipulator to remove the SLP Spacelab Pallet from Destiny at 1825 GMT. Meanwhile the EVA crew moved the DCSU switching unit from a sidewall carrier on the port side of Endeavour's cargo bay to the ESP (External Stowage Platform) on Destiny, next to the PFCS (Pump Flow Control System) which was installed on the ESP on the previous mission.
2002 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-26. -
Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
2002 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-26. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
2002 - Launch Site: Kodiak. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aries. LV Configuration: Aries QRLV-2. -
Target mission Nation: USA. Agency: USAF SMC. Apogee: 160 km (90 mi).
2003 - 04:23 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 410-02.
2005 - -
Landing of Soyuz TMA-5 Nation: Russia. Program: ISS. Flight: ISS EO-10, ISS EO-11, ISS EP-8. The EO-10 crew, having handed over the ISS to EO-11, boarded Soyuz TMA-5 together with EP-8 astronaut Vittori. They undocked from the ISS Zarya module at 18:45 GMT, made retrofire on schedule at 21:17, and landed on muddy ground at 51 deg 03" N / 67 deg 18" E at 22:07
2006 - 16:03 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz-U. LV Configuration: Soyuz-U P15000-100 / ISS-21P.
2007 - 06:48 GMT - Launch Site: Wallops Island. Launch Complex: LA0B. Launch Pad: -. Launch Vehicle: Minotaur. Model: Minotaur 1. LV Configuration: Minotaur 1 7. -
NFIRE Nation: USA. Payload: SA-200B. Mass: 494 kg (1,089 lb). Class: Technology. Spacecraft: SA-200. Manufacturer: Spectrum Astro. Agency: USAFRL. Perigee: 489 km (303 mi). Apogee: 497 km (308 mi). Inclination: 48.20 deg. Period: 94.50 min. COSPAR: 2007-014A. USAF Sat Cat: 31140. Near Field Infrared Experiment conducted by the US Missile Defense Agency. Its Track Sensor Payload included visible and short, medium and long wave infrared
sensors to observe missiles launched from the ground, and obtain basic data to distinguish between the missile and its hot rocket exhaust plume for application to anti-ballistic missile systems. Secondary payloads included Tesat, a German laser communications terminal, and its hydrazine propulsion system. This was used to maneuver the satellite from its initial 255 km x 465 km x 48.2 deg orbit to 489 km x 497 km by 18 May. The orbit was changed to 243 km x 487 km on 9 August and by 23 August was 219 km x 450 km. The satellite had a dry mass of 380 kg dry, was 2.7 m long and 1.3 m in diameter. The first major sensor test occurred when Minotaur II rocket TLV-7, was
fired at 08:30 GMT on 23 August from Vandenberg in NFIRE Mission 2a. The Minotaur II was aimed to pass within 4 and 20 km of the NFIRE satellite while its third stage motor burning, to allow NFIRE to get a close look at the rocket and its exhaust. The Missile Defense Agency reported that the experiment was successful.
Born on this day in:
- 1915 - George W Hoover. American Manager. Birth City: New Kensington. Birth State: Pennsylvania. Birth Country: USA.
- 1942 - Valeri Abramovich Voloshin. Russian Pilot Cosmonaut. Birth City: Yangiyul. Birth State: Tashkent. Birth Country: Uzbekistan.
- 1959 - Yvonne Darlene Cagle. American Mission Specialist Astronaut. Birth City: West Point. Birth State: New York. Birth Country: USA.
Died on this day in: - 1967 - Vladimir Mikhailovich Komarov
. Russian Pilot Cosmonaut. Cause of Death: Crash of Soyuz 1 spacecraft.
- 1998 - Mikhail Fedorovich Rebrov. Russian Journalist Cosmonaut. Cause of Death: Cancer.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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