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On June 4 in Space History
1954 June 4 - .
- X-1A Flight 17 - .
Crew: Murray.
Payload: X-1A flight 17. Nation: USA.
Related Persons: Murray.
Class: Manned.
Type: Manned rocketplane. Spacecraft Bus: XS-1.
Spacecraft: X-1A.
AF flight 11. X-1A reached 27374 m. Encountered same instability Yeager had, but at mach 1.97. Murray recovered after tumbling 6100 m down to 20130 m..
1954 June 4 - .
Launch Site:
Edwards.
LV Family:
Navaho.
Launch Vehicle:
Navaho X-10.
- Navaho X-10 flight 6 - .
Nation: USA.
Program: Navaho.
Planned supersonic flight aborted. Left main tire blew on takeoff run. Flight achieved, but the gear could not be retracted. Ground loop on landing, the vehicle sustained repairable damage..
1956 June 4 - .
14:13 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC35.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee Hi.
FAILURE: Failure.
- RV-N-13a test - .
Nation: USA.
Agency: NRL.
Apogee: 58 km (36 mi). Sunfollower spectrograph. Launched at 0713 local time. Reached 58 km..
1958 June 4 - .
15:15 GMT - .
Launch Site:
Holloman.
Launch Complex:
Holloman A.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee Hi.
- Solar extreme ultraviolet Spectrum Solar extreme ultraviolet mission - .
Nation: USA.
Agency: USAF.
Apogee: 200 km (120 mi).
1958 June 4 - .
21:17 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC18B.
Launch Pad: LC18B.
LV Family:
Thor.
Launch Vehicle:
Thor DM-18.
- Research and development Series III test - .
Nation: USA.
Agency: USAF.
Apogee: 520 km (320 mi).
The first Air Force Thor IRBM flight test missile (Number 115) to be fired from a tactical-type launcher was launched at Cape Canaveral. The missile completed a successful flight, impacting 1,170 nautical miles downrange. This was also the first Thor to be launched without a flight readiness firing of its propulsion system. USAF Thor flight tested for the first time from a tactical-type launcher at Cape Canaveral.
1959 June 4 - .
- Post-Mercury program using maneuverable Mercury spacecraft - .
Nation: USA.
Related Persons: Gilruth.
Program: Apollo.
Spacecraft: Mercury.
At an STG staff meeting, Director Robert R. Gilruth suggested that study should be made of a post-Mercury program in which maneuverable Mercury spacecraft would make land landings in limited areas..
1959 June 4 - .
- Mercury follow-on program using maneuverable Mercury capsules. - .
Nation: USA.
Related Persons: Gilruth.
Spacecraft Bus: Mercury.
Spacecraft: Mercury Mark I.
At a staff meeting, Space Task Group Director Robert R. Gilruth suggested studying a Mercury follow-on program using maneuverable Mercury capsules for land landings in predetermined areas. .
1959 June 4 - .
- OKB Filial 2 created. - .
Nation: Russia.
Decree 191 'On creation of OKB-1 Branch No. 2 at Krasnoyarsk-26 GKOT' was issued..
1959 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral AMR DZ.
Launch Pad: 29.0 N x 79.0 W.
Launch Platform: B-58.
Launch Vehicle:
High Virgo.
- High Virgo satellite interceptor mission - .
Nation: USA.
Agency: USAF.
Apogee: 51 km (31 mi).
1960 June 4 - .
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78.
- Molniya launch vehicle and initial Vostok flights approved. - .
Nation: Russia.
Spacecraft: Vostok.
Central Committee and Council of Soviet Ministers Decree 587-238 'On the Realisation of the Plan to Master Cosmic Space in 1960 and the First Half of 1961 -creation of a four-stage launcher for interplanetary missions and schedule for the Korabl-Sputniks'.
1960 June 4 - .
15:49 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Vehicle:
R-7.
- UBP (Readiness) operational test launch - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,350 km (830 mi). R-7 readiness verification test..
1961 June 4 - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
Launch Vehicle:
R-14.
- Nation: Russia.
Agency: RVSN.
Apogee: 675 km (419 mi).
1962 June 4 - .
Launch Site:
Reggane.
Launch Vehicle:
Veronique.
FAILURE: Failure.
- Aeronomy mission - .
Nation: France.
Agency: CNES.
Apogee: 100 km (60 mi).
1962 June 4 - .
09:44 GMT - .
Launch Site:
Johnston Island.
Launch Complex:
Johnston Island LE1.
LV Family:
Thor.
Launch Vehicle:
Thor DSV-2E.
- BLUEGILL Nuclear test - .
Nation: USA.
Agency: USAF.
Apogee: 500 km (310 mi).
Initial attempt to launch a live nuclear weapon using the Thor IRBM from Johnston Atoll. The range safety radar had been unreliable before launch,. Five minutes after launch, after shutdown of the booster, the Johnston missile tracking system failed. Unable to monitor the warhead's flight path, the range safety officer destroyed it 10 minutes later, prior to warhead detonation.
1963 June 4 - .
- The State Commission for Vostok 5/6 launches meets. - .
Nation: Russia.
Related Persons: Bykovsky,
Tereshkova.
Flight: Vostok 5,
Vostok 6.
Spacecraft: Vostok.
All is ready, but the wind is predicted to by 15 to 20 m/s on 7 June. The launch vehicle cannot be launched in winds over 15 m/s. Bykovskiy and Tereshkova are confirmed as the crew for 8 and 3 day flight durations. When they return to earth, a new and difficult life as celebrities will begin for them -- they will be known all over the world.
1963 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 601.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1963 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 601.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1963 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 601.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1963 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 601.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1963 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 601.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1963 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 601.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1963 June 4 - .
20:12 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg OSTF1.
LV Family:
Atlas.
Launch Vehicle:
Atlas E.
- Research and development launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,600 km (900 mi).
1964 June 4 - .
- Voskhod technical review - .
Nation: Russia.
Related Persons: Korolev.
Program: Voskhod.
Flight: Voskhod 1,
Voskhod 2.
Spacecraft Bus: Vostok.
Spacecraft: Voskhod.
Korolev presents the Voskhod technical design to organisations outside of OKB-1. Over 27 VVS representatives, including 10 cosmonauts, attend. The two Vostok variants have been dubbed 3KV (3-crew version) and 3KD (2 crew version with airlock). Korolev will complete integration of the first 3KV article by 12 June (8 days from the briefing). The first two articles will be shipped to Baikonur on 15 June for final test. An unmanned test flight with mannequins will be made in July, with the first three-crew manned flight in August. This will be followed by the first 3KD flight in September, with the first spacewalk. The difficulty in preparing equipment and training crews on this schedule are immense; and the chances of complete success are low. But it is the only way the Soviet Union can maintain its leadership in space in the face of the impending Gemini and Apollo flight tests, and the delays in Soyuz. After the meeting, Kamanin decides to train two cosmonauts as Voskhod spacecraft commanders, and the other three as spacewalkers.
1964 June 4 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78.
FAILURE: At T+104 sec the tank draining of core Block A failed due to jamming of the servo-motored throttle and break down of the motor's circuit The launcher was destroyed on impact downrange from the pad..
Failed Stage: 0.
- Molniya-1 s/n 2 Failure - .
Payload: Molniya-1 s/n 2. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: RVSN.
Program: Molniya.
Class: Communications.
Type: Military communications satellite. Spacecraft Bus: KAUR-2.
Spacecraft: Molniya-1.
Unsuccessful first attempt to launch Molniya communications satellite..
1964 June 4 - .
03:50 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC5.
LV Family:
Scout.
Launch Vehicle:
Scout X-4.
- Transit 5C-1 - .
Payload: Transit 5C / OPS 4412. Mass: 54 kg (119 lb). Nation: USA.
Agency: USN.
Program: Transit.
Class: Navigation.
Type: Navigation satellite. Spacecraft: Transit.
USAF Sat Cat: 801 . COSPAR: 1964-026A. Apogee: 898 km (557 mi). Perigee: 825 km (512 mi). Inclination: 90.50 deg. Period: 102.20 min. Operational prototype similar to the 5A series but with some redesign to improve performance. Operated successfully until 23 August 1965..
1964 June 4 - .
22:59 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC3W.
LV Family:
Thor.
Launch Vehicle:
Thor SLV-2A Agena D.
- KH-4A 1006 - .
Payload: KH-4A s/n 1006 / Agena D 1176 / OPS 3483. Mass: 1,500 kg (3,300 lb). Nation: USA.
Agency: CIA,
NRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-4A.
Decay Date: 1964-06-18 . USAF Sat Cat: 802 . COSPAR: 1964-027A. Apogee: 429 km (266 mi). Perigee: 149 km (92 mi). Inclination: 80.00 deg. Period: 90.30 min. KH-4A. Highest quality imagery attained to date from the KH-4 system..
1964 June 4 - .
23:44 GMT - .
Launch Site:
Woomera.
Launch Complex:
Woomera LA6A.
Launch Vehicle:
Blue Streak.
- Blue Streak only. Successful. - .
Nation: Europe.
Agency: ELDO.
Apogee: 157 km (97 mi).
1965 June 4 - .
- Birth of Shannon Walker - .
Nation: USA.
Related Persons: Walker, Shannon.
American astrophysicist mission specialist astronaut, 2004-on. 1 spaceflight, 163.3 days in space. Flew to orbit on Soyuz TMA-19 (2010)..
1966 June 4 - .
- Gemini 9 - Wakeup Song: The Lonely Bull - .
Flight: Gemini 9.
Spacecraft: Gemini.
"The Lonely Bull" by Tijuana Brass - From"The Last Man on the Moon". Copyright 1999 by Eugene Cernan and Don Davis. St. Martin's Press, LLC, New York, NY., p.124..
1966 June 4 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC41/3.
Launch Pad: LC41/3?.
LV Family:
R-16.
Launch Vehicle:
R-16U.
- Military training launch - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,210 km (750 mi).
1967 June 4 - .
- Birth of Robert Shane Kimbrough - .
Nation: USA.
Related Persons: Kimbrough.
American engineer mission specialist astronaut 2004-on. US Army 2 spaceflights, 189.0 days in space. Flew to orbit on STS-126 (2008), Soyuz MS-02..
1967 June 4 - .
- Death of Lloyd Viel Berkner - .
Nation: USA.
Related Persons: Berkner.
American engineer. Leading organiser of the International Geophysical Year in 1957-1958.
1967 June 4 - .
18:10 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC4E.
LV Family:
Atlas.
Launch Vehicle:
Atlas SLV-3 Agena D.
- KH 7-38 - .
Payload: KH-7 no. 38 / OPS 4360. Mass: 2,000 kg (4,400 lb). Nation: USA.
Agency: NRO,
USAF.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: WS-117.
Spacecraft: KH-7.
Decay Date: 1967-06-12 . USAF Sat Cat: 2831 . COSPAR: 1967-055A. Apogee: 456 km (283 mi). Perigee: 149 km (92 mi). Inclination: 104.90 deg. Period: 90.60 min. The final Air Force Atlas/Agena D (SLV-3 #7128/SS-01B #4837) was successfully launched from Vandenberg AFB. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
1968 June 4 - .
- New AAP schedule decreased to 11 Saturn IB flights and one Saturn V flight. - .
Nation: USA.
Spacecraft: AES Lunar Base,
ALSS Lunar Base,
Orbital Workshop,
Skylab.
NASA released a new AAP launch readiness and delivery schedule. The schedule decreased the number of Saturn flights to 11 Saturn IB flights and one Saturn V flight. It called for three Workshops. One of the Workshops would be launched by a Saturn IB, and another would serve as a backup. The third Workshop would be launched by a Saturn V. The schedule also included one ATM. Launch of the first Workshop would be in November 1970. Lunar missions were no longer planned in the AAP.
1968 June 4 - .
06:43 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
FAILURE: Launch vehicle failed to orbit - unknown cause..
Failed Stage: U.
- Sfera s/n 12L - .
Mass: 800 kg (1,760 lb). Nation: Russia.
Agency: RVSN.
Spacecraft Bus: KAUR-1.
Spacecraft: Sfera.
1968 June 4 - .
06:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 224 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-06-12 . USAF Sat Cat: 3276 . COSPAR: 1968-046A. Apogee: 256 km (159 mi). Perigee: 203 km (126 mi). Inclination: 51.80 deg. Period: 89.10 min. High resolution photo reconnaissance satellite; returned film capsule; also measured atmospheric composition..
1968 June 4 - .
16:37 GMT - .
Launch Site:
White Sands.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Recovery test - .
Nation: USA.
Agency: NASA.
Apogee: 130 km (80 mi).
1970 June 4 - .
- Soyuz 9 Day 4 - .
Nation: Russia.
Related Persons: Mishin,
Nikolayev,
Sevastyanov,
Tereshkova,
Tregub.
Program: Soyuz.
Flight: Soyuz 9.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-OK.
There are a total of 500 staff at Yevpatoriya for the mission, including 53 representatives from the VVS, 6 military cosmonauts, and 3 civilian cosmonauts. Mishin returns to Moscow, leaving Tregub in his place. In the afternoon there is a problem with the control of the spacecraft's solar cells. On the 47th orbit Sevastyanov reports that one solar panel is energised, but only generating 26 amps. This could only mean that the automatic control of the solar panels was not working. On the second day the crew had to engage and disengage the solar batteries 12 times manually. After the 15th manual session it became clear that the mission could last only eight days before the batteries would run down. In the orbit of Soyuz 9 in June, the night lasts 40 minutes. On the previous flight, in October, it lasted only 10 minutes and this would not have been a problem. The crew is told to revolve the spacecraft at 0.5 deg/sec around the long axis. By this method the spacecraft remains fully oriented towards the sun, and the batteries don't have to work so long on the night passes. The cosmonauts do not report any unpleasant sensations from the rotation. At the 23:25 communications sessions the cosmonauts report that their appetites are good and they are sleeping well.
1970 June 4 - .
1971 June 4 - .
- Backup crew named to fly Soyuz 11 - .
Nation: Russia.
Related Persons: Dobrovolsky,
Kolodin,
Leonov,
Mishin,
Patsayev,
Rukavishnikov,
Volkov.
Program: Salyut.
Flight: Soyuz 11,
Soyuz 12 / DOS 1.
Soyuz 11 is on the launch pad, and which crew will fly is still being argued. Kamanin wants to simply have Volkov replace Kubasov on Leonov's crew. Mishin wants the complete backup crew to replace Leonov's crew. Others on the launch commission support Mishin. At 15:30 a team of physicians arrive from Moscow to verify the diagnosis of Kubasov. At 18:00 the final state commission meeting confirms the Dobrovolsky crew. At 19:00 a press conference is held - Dobrovolsky, Patsayev, and Volkov are publicly presented as the crew of Soyuz 11.
1971 June 4 - .
- X-24 Flight 28 - .
Crew: Manke.
Payload: X-24A flight 28. Nation: USA.
Related Persons: Manke.
Class: Manned.
Type: Manned spaceplane. Spacecraft Bus: X-24.
Spacecraft: X-24A.
Final X-24A flight. Maximum Speed - 867 kph. Maximum Altitude - 16581 m. Flight Time - 517 sec..
1971 June 4 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF04.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 2.
- OT GT81M operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1971 June 4 - .
18:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 426 - .
Payload: DS-U2-K s/n 1. Mass: 680 kg (1,490 lb). Nation: Russia.
Agency: MO.
Program: DS.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft Bus: DS.
Spacecraft: DS-U2-K.
Completed Operations Date: 1972-01-12 . Decay Date: 2002-05-11 . USAF Sat Cat: 5281 . COSPAR: 1971-052A. Apogee: 1,108 km (688 mi). Perigee: 354 km (219 mi). Inclination: 74.00 deg. Period: 99.40 min. Studied charged particle flows and cosmic radiation..
1973 June 4 - .
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Missile Suspension Systems - .
The Boeing Company was awarded a $50.4 million contract for the Missile Suspension Systems (MSS) for Wings III, VI, and Squadron 20..
1973 June 4 - .
17:10 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC36.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant VC.
FAILURE: Failure.
- CALROC 1 Solar extreme ultraviolet mission - .
Nation: USA.
Agency: NASA.
Apogee: 132 km (82 mi).
1974 June 4 - .
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- Shuttle Enterprise construction begins. - .
Nation: USA.
Program: STS.
Spacecraft Bus: Shuttle.
Spacecraft: Enterprise.
Structural assembly of the crew module for shuttle Enterprise (OV-101) begins at Plant 42 in Palmdale..
1974 June 4 - .
- Structural assembly of crew module for OV-102 begun. - .
Nation: USA.
Program: STS.
Class: Manned.
Type: Manned spaceplane. Spacecraft Bus: Shuttle.
Spacecraft: Columbia.
1975 June 4 - .
Launch Site:
Wallops Island.
- The sixth and last flight of the Pedro Recruit sounding rockets for the FLAME program occurred at Wallops Island, Virginia. - .
The sixth and last flight of the Pedro Recruit sounding rockets for the FLAME program occurred at Wallops Island, Virginia..
1975 June 4 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC101.
LV Family:
R-36M.
Launch Vehicle:
R-36M 15A14.
- SLI? - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
1976 June 4 - .
04:23 GMT - .
Launch Site:
South Uist.
Launch Vehicle:
Petrel.
- E field / VLF Ionosphere mission - .
Nation: UK.
Agency: SRC.
Apogee: 143 km (88 mi).
1976 June 4 - .
04:39 GMT - .
Launch Site:
South Uist.
Launch Vehicle:
Petrel.
- VLF Ionosphere mission - .
Nation: UK.
Agency: SRC.
Apogee: 132 km (82 mi).
1979 June 4 - .
14:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC43.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Nation: USA.
Agency: MRN.
Apogee: 85 km (52 mi).
1980 June 4 - .
07:34 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Vostok 8A92M.
- Cosmos 1184 - .
Payload: Tselina-D no. 25. Mass: 3,800 kg (8,300 lb). Nation: Russia.
Agency: MOM.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-D.
Decay Date: 2002-04-29 . USAF Sat Cat: 11821 . COSPAR: 1980-044A. Apogee: 535 km (332 mi). Perigee: 532 km (330 mi). Inclination: 81.20 deg. Period: 95.30 min.
1981 June 4 - .
15:41 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 1275 - .
Mass: 810 kg (1,780 lb). Nation: Russia.
Agency: MO.
Class: Navigation.
Type: Navigation satellite. Spacecraft Bus: KAUR-1.
Spacecraft: Parus.
Decay Date: 1981-09-30 . USAF Sat Cat: 12504 . COSPAR: 1981-053A. Apogee: 1,005 km (624 mi). Perigee: 954 km (592 mi). Inclination: 83.00 deg. Period: 104.70 min. Military navigation satellite. Replaced Cosmos 1141..
1982 June 4 - .
18:55 GMT - .
Launch Site:
Point Mugu.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Nation: USA.
Agency: MRN.
Apogee: 93 km (57 mi).
1983 June 4 - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-200.
- Nation: India.
Agency: ISRO.
Apogee: 60 km (37 mi).
1984 June 4 - .
14:20 GMT - .
Launch Site:
Balasore.
LV Family:
RH.
Launch Vehicle:
RH-200.
- Meteorological Chaff Meteorological mission - .
Nation: India.
Agency: ISRO.
Apogee: 67 km (41 mi).
1985 June 4 - .
00:33 GMT - .
Launch Site:
Kwajalein.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Arcasonde - .
Nation: USA.
Agency: MRN.
Apogee: 80 km (49 mi).
1986 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 620.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1986 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 620.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1986 June 4 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 620.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1986 June 4 - .
21:34 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 620.
LV Family:
Polaris.
Launch Vehicle:
Poseidon C3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 500 km (310 mi).
1987 June 4 - .
18:50 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC16/2.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Cosmos 1849 - .
Payload: Oko #53. Mass: 1,800 kg (3,900 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: Oko.
Decay Date: 2003-02-04 . USAF Sat Cat: 18083 . COSPAR: 1987-048A. Apogee: 37,311 km (23,183 mi). Perigee: 3,104 km (1,928 mi). Inclination: 67.10 deg. Period: 719.00 min. Covered Oko constellation plane 1 - 274 degree longitude of ascending node..
1988 June 4 - .
Launch Site:
Thumba.
LV Family:
RH.
Launch Vehicle:
RH-200.
- Meteorological Chaff Meteorological mission - .
Nation: India.
Agency: ISRO.
Apogee: 70 km (43 mi).
1989 June 4 - .
Launch Vehicle:
MAKS.
- An-225 / Buran displayed at Paris Air Show. - .
Nation: Russia.
Program: Buran.
Spacecraft: Buran.
1991 June 4 - .
08:10 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32/2.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Okean 3 - .
Payload: Okean-O1 no. 6. Mass: 1,950 kg (4,290 lb). Nation: Russia.
Agency: MOM.
Program: Okean.
Class: Earth.
Type: Civilian Radarsat. Spacecraft: Okean-O1.
Completed Operations Date: 1994-01-04 . USAF Sat Cat: 21397 . COSPAR: 1991-039A. Apogee: 656 km (407 mi). Perigee: 621 km (385 mi). Inclination: 82.50 deg. Period: 97.50 min. Oceanography. Gathering of up-to-date oceanographic information and data on ice conditions in the interests of the Soviet economy and international cooperation. Okean 3 ceased working in January of 1994..
1993 June 4 - .
Launch Site:
Anhueng.
LV Family:
KSR.
Launch Vehicle:
KSR-I.
- Ozone profile mission - .
Nation: Korea South.
Agency: KARI.
Apogee: 39 km (24 mi). Ultraviolet radiometer to measure vertical ozone distribution in the stratosphere over the Korean peninsula. Rocket performance also monitored..
1994 June 4 - .
Launch Site:
Balasore.
LV Family:
S-75.
Launch Vehicle:
Prithvi.
- Test mission - .
Nation: India.
Agency: IDRDL.
Apogee: 100 km (60 mi).
1996 June 4 - .
05:06 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC36.
Launch Pad: LC36 Athena.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant 8C.
- XQC F2 X-ray astronomy mission - .
Nation: USA.
Agency: NASA Greenbelt.
Apogee: 220 km (130 mi).
1996 June 4 - .
12:34 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5G.
FAILURE: Vehicle went off course and was destroyed by range safety. Reuse of flight software from Ariane 4 was the cause (faulty program logic that only took effect on Ariane 5 launch trajectory)..
Failed Stage: G.
- Cluster F2 - .
Nation: Europe.
Agency: ESA.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Cluster.
- Cluster F3 - .
Nation: Europe.
Agency: ESA.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Cluster.
- Cluster F4 - .
Nation: Europe.
Agency: ESA.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Cluster.
1997 June 4 - .
09:00 GMT - .
Launch Site:
Kiruna.
LV Family:
Hawk.
Launch Vehicle:
Improved Orion.
- Test mission - .
Nation: Sweden.
Agency: SSC.
Apogee: 94 km (58 mi).
1998 June 4 - .
- STS-91 - Wakeup Song: Come Go With Me - .
Flight: STS-91.
"Come Go With Me" by the Del Vikings in honor of Andrew Thomas' return from Mir CAPCOM: Marc Garneau.
1999 June 4 - .
1999 June 4 - .
- STS-96 - Wakeup Song: Good Morning Starshine - .
Flight: STS-96.
"Good Morning Starshine" in recognition of the deployment of the Starshine satellite..
2002 June 4 - .
- Mars Odyssey, Deployment of GRS Boom, Successful - .
Nation: USA.
Spacecraft: Mars Odyssey.
2003 June 4 - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2398 - .
Mass: 820 kg (1,800 lb). Nation: Russia.
Agency: VKS.
Manufacturer: Reshetnev bureau.
Class: Navigation.
Type: Navigation satellite. Spacecraft Bus: KAUR-1.
Spacecraft: Parus.
USAF Sat Cat: 27818 . COSPAR: 2003-023A. Apogee: 1,016 km (631 mi). Perigee: 970 km (600 mi). Inclination: 83.00 deg. Period: 105.00 min.
2004 June 4 - .
Launch Site:
Tilla.
LV Family:
Nodong 1.
Launch Vehicle:
Ghauri.
- Test mission - .
Nation: Pakistan.
Apogee: 150 km (90 mi).
2008 June 4 - .
- STS-124 MCC Status Report #08 - .
Nation: USA.
Program: ISS.
Flight: STS-124.
The crew of STS-124 and Expedition 17 will focus on continuing the setup and initialization of the Kibo laboratory today. .
Additional Details: here....
2008 June 4 - .
- STS-124 - Wakeup Song: Have You Ever - .
Flight: STS-124.
"Have You Ever" performed by Brandi Carlile. The song was played for Mission Specialist Karen Nyberg..
2010 June 4 - .
18:45 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
Launch Pad: SLC40.
LV Family:
Falcon.
Launch Vehicle:
Falcon 9.
- Dragon/Falcon 9 - .
Mass: 4,000 kg (8,800 lb). Nation: USA.
Agency: SpaceX.
Class: Manned.
Type: Manned spacecraft. Spacecraft: Dragon.
Duration: 23.00 days. Decay Date: 2010-06-27 . USAF Sat Cat: 36595 . COSPAR: 2010-026A. Apogee: 140 km (80 mi). Perigee: 138 km (85 mi). Inclination: 34.50 deg. Period: 87.30 min. First launch of the commercial Falcon 9 launch vehicle. Structural model of Dragon reusable spacecraft. Remained attached to final stage..
2016 June 4 - .
14:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC133/3.
LV Family:
UR-100N.
Launch Vehicle:
Rokot.
- Cosmos 2517 - .
Nation: Russia.
Class: Earth.
Type: Geodetic satellite. Spacecraft Bus: KAUR-1.
Spacecraft: Geo-IK.
USAF Sat Cat: 41579 . COSPAR: 2016-034A. Apogee: 961 km (597 mi). Perigee: 936 km (581 mi). Inclination: 99.30 deg. 0600LT SSO. Russian earth geodetic satellite..
2018 June 4 - .
04:44 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Falcon.
Launch Vehicle:
Falcon 9.
- SES-12 - .
Nation: SES.
USAF Sat Cat: 43488 . COSPAR: 2018-049A. Apogee: 35,864 km (22,284 mi). Perigee: 35,842 km (22,271 mi). Inclination: 0.0600 deg. Period: 1,439.47 min. See SES 12. ..
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