Encyclopedia Astronautica
November 04


November 04 Chronology


1908 November 4 - .
  • Birth of Louis G Dunn - . Nation: USA. Summary: American engineer. At Ramo-Woolridge headed oversight of development of the Thor, Titan, Atlas, and Minuteman missiles for the USAF.

1918 November 4 - .
  • Birth of Werner Baum - . Nation: Germany; Russia. Summary: German engineer, member of Rocket Team in the Soviet Union after WW2. Worked on rocket engine development in Glushko's design bureau from 1947 to 1952 as Deputy of the Chief and Technical Designer; Dept. 61..

1919 November 4 - .
  • Birth of Oskar F Holderer - . Nation: Germany; USA. Summary: German engineer in WW2, member of the Rocket Team in the United States thereafter..

1944 November 4 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 19495.
  • V-2 Ma253 221 K5 - . Nation: Germany. Summary: Planned range 225 km. Impact 3.3 km to the right of the planned trajectory. Circular error 3.4 km from aim point..

1947 November 4 - .
  • XS-1 Flight 57 - . Crew: Yeager. Payload: XS-1 # 1 flight 37. Nation: USA. Related Persons: Yeager. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF flight 15..

1947 November 4 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Corporal. Launch Vehicle: Corporal E. LV Configuration: Corporal E 3.
  • Test mission - . Nation: USA. Agency: USA OR. Apogee: 20 km (12 mi).

1947 November 4 - . 15:02 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: V-2. Launch Vehicle: A-4. LV Configuration: A-4 01T.
  • Soviet V-2 launch - . Nation: USSR. Agency: Korolev. Apogee: 89 km (55 mi). Summary: Range achieved 268 km. Met objectives..

1948 November 4 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1. LV Configuration: R-1 I-2.
  • Test mission - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1952 November 4 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-2353.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1953 November 4 - . Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: Honest John. LV Configuration: Honest John 2DJ.
  • Test mission - . Nation: USA. Apogee: 10 km (6 mi).

1954 November 4 - .
  • X-1B Flight 8 - . Crew: Harer. Payload: X-1B flight 7. Nation: USA. Related Persons: Harer. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1B. Summary: AF flight 7..

1955 November 4 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1E. LV Configuration: R-1E 3.
  • Biological mission - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi). Summary: Payload, instruments, left and right animal containers all recovered. Smoke container functioned. Carried dogs..

1955 November 4 - . 15:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-N-10c. LV Configuration: Aerobee RTV-N-10c NRL 36.
  • Solar La / airglow Solar ultraviolet mission - . Nation: USA. Agency: NRL. Apogee: 135 km (83 mi). Summary: Solar spectrum research. Launched at 0830 local time. Reached 158 km..

1956 November 4 - .
  • Soviet troops enter and reclaim Budapest - . Nation: USSR.

1956 November 4 - . 18:54 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 58.0 N x 47.0 W. Launch Platform: LSD-14. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun N-C 10.
  • UM AM6.10 Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 162 km (100 mi). Summary: Launched during University of Michigan's 1956 Cruise 1956 at Launch Point 3 - - Latitude: 58.00 N - Longitude: 47.00 W..

1957 November 4 - . 01:41 GMT - . Launch Site: Pacific Ocean. Launch Pad: 71.2 S x 176.1 E. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon SUI 101.
  • II5.77F Aeronomy / Fields mission - . Nation: USA. Agency: SUI. Apogee: 113 km (70 mi).

1957 November 4 - . 03:47 GMT - . Launch Site: Pacific Ocean. Launch Pad: 71.5 S x 176.8 E. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon SUI 102.
  • II5.78F Aeronomy / Fields mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

1957 November 4 - . 07:16 GMT - . Launch Site: Pacific Ocean. Launch Pad: 72.0 S x 176.7 E. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon SUI 103.
  • II5.79F Aeronomy / Chemical release mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

1957 November 4 - . 18:52 GMT - . Launch Site: Pacific Ocean. Launch Pad: 70.9 S x 173.6 E. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon SUI 104.
  • II5.80F Aeronomy / Fields mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

1958 November 4 - . 16:50 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun OB6.12.
  • Arctic cloud cover Meteorological / imaging mission - . Nation: USA. Agency: USAF. Apogee: 122 km (75 mi).

1959 November 4 - . 14:30 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA1. LV Family: Little Joe. Launch Vehicle: Little Joe 1 2P. LV Configuration: Little Joe 1-2P LJ-1A.
  • Mercury LJ-1A - . Nation: USA. Agency: NASA. Apogee: 14 km (8 mi). Little Joe 1-A (LJ-1A) was launched in a test for a planned abort under high aerodynamic load conditions. This flight was a repeat of the Little Joe (LJ-1) that had been planned for August 21, 1959 (escape rocket fired 31 min before the intended launch of the Little Joe launch vehicle). After lift-off, the pressure sensing system was to supply a signal when the intended abort dynamic pressure was reached (about 30 sec after launch). An electrical impulse was then sent to the explosive bolts to separate the spacecraft from the launch vehicle. Up to this point, the operation went as planned, but the impulse was also designed to start the igniter in the escape motor. The igniter activated, but pressure failed to build up in the motor until a number of seconds had elapsed. Thus the abort maneuver, the prime mission of the flight, was accomplished at a dynamic pressure that was too low. For this reason a repeat of the test was planned. All other events from the launch through recovery occurred without incident. The flight attained an altitude of 9 statute miles, a range of 11.5 statute miles, and a speed of 2,021.6 miles per hour.

1959 November 4 - . 21:37 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC13. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 28D.
  • Research and development launch - . Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi).

1960 November 4 - . 20:43 GMT - . Launch Site: Palmdale Omni DZ. Launch Pad: 34.7 N x 118.0 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-16-29.
  • X-15A Stability/Control test - . Nation: USA. Agency: NASA; USAF. Apogee: 14 km (8 mi). Summary: Maximum Speed - 2071 kph. Maximum Altitude - 14905 m..

1962 November 4 - .
  • Mercury veteran Enos dies - . Nation: USA. Program: Mercury. Enos, the 6-year-old chimpanzee who made a two-orbit flight around the earth aboard the Mercury-Atlas 5 (MA-5) spacecraft (November 29, 1961, entry) died at Holloman Air Force Base, New Mexico. The chimpanzee had been under night and day observation and treatment for 2 months before his death. He was afflicted with shigella dysentary, a type resistant to antibiotics, and this caused his death. Officials at the Air Medical Research Laboratory stated that his illness and death were in no way related to his orbital flight the year before.

1962 November 4 - . 07:15 GMT - . Launch Site: Johnston Island. LV Family: Nike Hercules. Launch Vehicle: Nike Hercules.
  • DOMINIC TIGHTROPE Nuclear test - . Nation: USA. Agency: USAF. Apogee: 24 km (14 mi). This was a DOD sponsored live test of the Nike Hercules air defense missile system. The low-kiloton range W-31 warhead detonated at 21 km altitude 3 km SSW of Johnston Atoll. This was the last U.S. atmospheric test. On Johnston Island an intense white flash was accompanied by a strong heat pulse. A yellow-orange disc formed, slowly changing to a purple toroid which faded from view after several minutes.

1962 November 4 - . 15:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78. LV Configuration: Molniya 8K78 T103-17. FAILURE: After T+260 sec, a malfunction of the pressurization system of the central sustainer led to cavitation in the oxidizer pipeline and LOX pump, followed at T+292s by the fuel pump.. Failed Stage: 1.
  • Sputnik 24 - . Payload: 2MV-3 s/n 1. Mass: 890 kg (1,960 lb). Nation: USSR. Agency: RVSN. Program: Mars. Class: Venus. Type: Venus probe. Spacecraft: Mars 2MV-3. Decay Date: 1962-11-05 . USAF Sat Cat: 451 . COSPAR: 1962-B-Xi-1. Apogee: 170 km (100 mi). Perigee: 170 km (100 mi). Inclination: 64.8000 deg. Period: 87.90 min. Mars probe intended to make a soft landing on Mars. Although the escape stage and payload reached orbit, the strong third stage vibrations shook a fuse loose from its mount in the main nozzle of the escape stage Block L's engine. The engine could not be ignited and remained in Earth orbit. It decayed about two months after insertion.

1963 November 4 - . Launch Site: Vandenberg.
  • First launch in the ABRES program - . Nation: USA. Summary: First launch in the Advanced Ballistic Reentry System (ABRES) program at Vandenberg AFB. Vehicle used for this mission was an Atlas D..

1963 November 4 - . 09:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 232D.
  • ABRES REX-III re-entry vehicle test flight - . Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).

1963 November 4 - . 10:00 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache Sphere.
  • Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 215 km (133 mi).

1963 November 4 - . 15:10 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 KP3.3.
  • Dayglow Aeronomy mission - . Nation: USA. Agency: KPNO. Apogee: 200 km (120 mi).

1964 November 4 - . LV Family: DF-2. Launch Vehicle: DF-2A.
  • Go-ahead for DF-2A. - . Nation: China. Related Persons: Tsien. Program: Long March. Summary: Decision to proceed with DF-2A extended range version of DF-2.

1964 November 4 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 537.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 November 4 - . 02:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1E. LV Family: Delta. Launch Vehicle: Thor Agena D SLV-2A/D. LV Configuration: Thor SLV-2A Agena D 430 / Agena D SS-01A 2317.
  • OPS 3062 - . Payload: Ferret 7 / Agena D 2317. Mass: 1,500 kg (3,300 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Ferret. Decay Date: 1969-11-05 . USAF Sat Cat: 922 . COSPAR: 1964-072A. Apogee: 526 km (326 mi). Perigee: 512 km (318 mi). Inclination: 82.0000 deg. Period: 95.00 min.

1964 November 4 - . 08:31 GMT - . Launch Site: CELPA. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C78.
  • Aeronomy mission - . Nation: France. Agency: CONAE. Apogee: 175 km (108 mi).

1964 November 4 - . 16:35 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique AGI53.
  • Solar La Solar ultraviolet mission - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi). Summary: FU110 Atomic H (Ly-alpha), Solar X-rays mission..

1964 November 4 - . 17:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-D. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II B-32.
  • High Rider - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). Summary: Demonstration and shakedown operations launch.

1965 November 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/3. Launch Pad: LC41/3?. LV Family: R-16. Launch Vehicle: R-16U.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1965 November 4 - . 05:31 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC86/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 95 - . Payload: DS-U2-V s/n 2. Mass: 325 kg (716 lb). Nation: USSR. Agency: MO. Program: DS. Class: Technology. Type: Military technology satellite. Spacecraft: DS-U2-V. Completed Operations Date: 1965-11-04 . Decay Date: 1966-01-18 . USAF Sat Cat: 1706 . COSPAR: 1965-088A. Apogee: 521 km (323 mi). Perigee: 211 km (131 mi). Inclination: 48.4000 deg. Period: 91.90 min. Summary: Military technology development satellite - mission still classified..

1965 November 4 - . 17:11 GMT - . Launch Site: Hidden Hills DZ. Launch Pad: 36.1 N x 116.0 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-62-103. FAILURE: Two engine relights required..
  • X-15A Checkout mission - . Nation: USA. Agency: NASA; USAF. Apogee: 24 km (14 mi). Summary: Maximum Speed - 4450 kph. Maximum Altitude - 24440 m..

1966 November 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/3. LV Family: R-16. Launch Vehicle: R-16U.
  • Combat training launch - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1966 November 4 - . 02:05 GMT - . Launch Site: Kagoshima. LV Family: S. Launch Vehicle: S-300 ISAS. LV Configuration: S-300 PT-300-1.
  • Test mission - . Nation: Japan. Agency: ISAS. Apogee: 160 km (90 mi).

1966 November 4 - . 08:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC161. Launch Pad: LC161/1. LV Family: RT-2. Launch Vehicle: RT-2.
  • Test mission - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1966 November 4 - . 15:16 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 164 km (101 mi).

1967 November 4 - .
  • Manned Soyuz flight by May 1968? - . Nation: USSR. Related Persons: Mishin. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Summary: Discussion on the Il-18 on the way back to Moscow from Tyuratam. Mishin thinks that a manned flight aboard Soyuz will be possible by April-May of 1968; the others don't think it can happen until the second half of the year..

1967 November 4 - . LV Family: Saturn I; Saturn V.
  • Apollo mission schedule for six flights in 1968 and five in 1969 - . Nation: USA. Related Persons: Mueller. Program: Apollo. Flight: Apollo 10; Apollo 14. Spacecraft: Apollo LM; CSM Recovery. NASA announced an Apollo mission schedule calling for six flights in 1968 and five in 1969. NASA Associate Administrator for Manned Space Flight George E. Mueller said the schedule and alternative plans provided a schedule under which a limited number of Apollo command and service modules and lunar landing modules, configured for lunar landing might be launched on test flights toward the moon by the end of the decade. Apollo/uprated Saturn I flights were identified with a 200 series number; Saturn V flights were identified with a 500 series number. Additional Details: Apollo mission schedule for six flights in 1968 and five in 1969.

1968 November 4 - . 08:03 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Agency: GMS. Apogee: 65 km (40 mi).

1969 November 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC142/34. LV Family: Tsiklon. Launch Vehicle: R-36 8K67P.
  • OS-67 No. 1L test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1969 November 4 - . 11:59 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 308 - . Payload: DS-P1-I s/n 7. Mass: 325 kg (716 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-I. Completed Operations Date: 1970-01-04 . Decay Date: 1970-01-04 . USAF Sat Cat: 4219 . COSPAR: 1969-096A. Apogee: 408 km (253 mi). Perigee: 271 km (168 mi). Inclination: 71.0000 deg. Period: 91.30 min. Summary: Operational radar target for the ABM forces..

1969 November 4 - . 19:29 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.136DS.
  • NRL NE3.215 FDVU Solar extreme ultraviolet mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1969 November 4 - . 20:27 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.283CS.
  • Solar x-ray mission - . Nation: USA. Agency: NASA. Apogee: 181 km (112 mi). The rockets achieved expected performance, solar pointing systems functioned properly, payloads were successfully recovered, and preliminary results appeared excellent. The information obtained by the rocket flights on solar emission intensity, filter performance, film response, and exposure time would be available in time to provide a useful and effective feedback into the ATM instruments development program.

1969 November 4 - . 22:38 GMT - . Launch Site: Fort Churchill. LV Family: Javelin. Launch Vehicle: Nike Javelin.
  • BRL 7 Ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 125 km (77 mi).

1969 November 4 - . 22:50 GMT - . Launch Site: Fort Churchill. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.893.
  • Polar Cap N-5 Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 143 km (88 mi).

1969 November 4 - . 23:08 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 5A. LV Configuration: Black Brant VA CRL AJ17.617.
  • Polar Cap U-6 Plasma mission - . Nation: USA. Agency: AFCRL. Apogee: 126 km (78 mi).

1970 November 4 - . 09:05 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-1W.
  • STM-1W research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 November 4 - . 16:00 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 636. Launch Vehicle: Poseidon.
  • Demonstration and shakedown operations surface launch - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1972 November 4 - . 02:15 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.487UA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 123 km (76 mi).

1972 November 4 - . 23:27 GMT - . Launch Site: CELPA. LV Family: Canopus. Launch Vehicle: Rigel.
  • MPE Barium release? EXP 64 Aeronomy / ionosphere mission - . Nation: Argentina. Agency: CONAE. Apogee: 252 km (156 mi).

1973 November 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 November 4 - . 10:40 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511M.
  • Cosmos 693 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MT. Duration: 12.00 days. Decay Date: 1974-11-16 . USAF Sat Cat: 7509 . COSPAR: 1974-088A. Apogee: 243 km (150 mi). Perigee: 219 km (136 mi). Inclination: 81.3000 deg. Period: 89.10 min. Summary: Military topography satellite; returned film capsule; separated science capsule..

1975 November 4 - . 10:13 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-275.
  • Cosmos 778 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 8419 . COSPAR: 1975-103A. Apogee: 1,001 km (621 mi). Perigee: 968 km (601 mi). Inclination: 83.0000 deg. Period: 104.80 min. Summary: Military navigation satellite..

1975 November 4 - . 15:20 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 779 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MK. Duration: 14.00 days. Decay Date: 1975-11-18 . USAF Sat Cat: 8420 . COSPAR: 1975-104A. Apogee: 341 km (211 mi). Perigee: 182 km (113 mi). Inclination: 62.8000 deg. Period: 89.70 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1976 November 4 - .
  • Complete 747 shuttle carrier aircraft modification - . Nation: USA. Program: STS.

1976 November 4 - . 07:45 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 6 AC. LV Configuration: Skylark 6 AC SL1306.
  • Large Area PC X-ray astronomy mission - . Nation: UK. Agency: BAC. Apogee: 191 km (118 mi).

1977 November 4 - .
  • Deliver aft fuselage on dock, Palmdale, Columbia - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Columbia.

1979 November 4 - . 10:40 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • - . Nation: USA. Agency: MRN. Apogee: 79 km (49 mi).

1980 November 4 - . 15:04 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 1220 - . Mass: 3,000 kg (6,600 lb). Nation: USSR. Agency: MO. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-P. Decay Date: 1982-06-20 . USAF Sat Cat: 12054 . COSPAR: 1980-089A. Apogee: 759 km (471 mi). Perigee: 526 km (326 mi). Inclination: 65.0000 deg. Period: 97.60 min. Summary: Ocean monitoring..

1981 November 4 - . 05:31 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/D-1. LV Configuration: Proton-K/D-1 311-02.
  • Venera 14 - . Payload: 4V-1 s/n 761. Mass: 4,000 kg (8,800 lb). Nation: USSR. Agency: MOM. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft: Venera 4V-1. USAF Sat Cat: 12938 . COSPAR: 1981-110A. Venera 13 and 14 were identical spacecraft built to take advantage of the 1981 Venus launch opportunity and launched 5 days apart. After launch and a four month cruise to Venus, the descent vehicle separated and plunged into the Venus atmosphere on 5 March 1982. As it flew by Venus the bus acted as a data relay for the brief life of the descent vehicle, and then continued on into a heliocentric orbit. The parachute of the descent vehicle opened after the lander reached subsonic speed. At an altitude of about 50 km the parachute was released and simple airbraking was used the rest of the way to the surface. Venera 14 landed about 950 km southwest of Venera 13 near the eastern flank of Phoebe Regio at 13 deg 15 min S by 310 E on a basaltic plain. After landing an imaging panorama was started It has been reported that the surface analysis arm accidentally landed on one of the ejected camera covers and therefore didn't send back any data on the Venusian soil. This is visible in photographs sent back. On the other hand, the official account very specifically states that the mechanical drilling arm obtained a sample, which was deposited in a hermetically sealed chamber, maintained at 30 degrees C and a pressure of about .05 atmospheres. The composition of the sample was determined by the X-ray flourescence spectrometer, showing it to be similar to oceanic tholeiitic basalts. The lander survived for 57 minutes (the planned design life was 32 minutes) in an environment with a temperature of 465 degrees C and a pressure of 94 Earth atmospheres.

1982 November 4 - . 15:46 GMT - . Launch Site: White Sands. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 57 km (35 mi).

1983 November 4 - . 16:30 GMT - . Launch Site: Primrose Lake. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 61 km (37 mi).

1985 November 4 - . 14:38 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1986 November 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 644. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1986 November 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 644. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1986 November 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 644. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1986 November 4 - . 11:50 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1790 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 14.00 days. Decay Date: 1986-11-18 . USAF Sat Cat: 17056 . COSPAR: 1986-085A. Apogee: 286 km (177 mi). Perigee: 191 km (118 mi). Inclination: 72.9000 deg. Period: 89.30 min. Summary: Military cartographic satellite; returned film capsule..

1986 November 4 - . 20:44 GMT - . Launch Site: Kiruna. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion SSC S41H.
  • Aureld-VIP-HIGH Auroral mission - . Nation: USA. Agency: SSC. Apogee: 206 km (128 mi).

1986 November 4 - . 20:59 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 644. Launch Vehicle: Poseidon.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1987 November 4 - . 13:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1988 November 4 - . 14:20 GMT - . Launch Site: Zingst. Launch Vehicle: MMR-06.
  • MMR06-M Zingst launch 3 - . Nation: USSR. Agency: GMS. Apogee: 43 km (26 mi). Summary: Test launch. Earth impacted at 250 seconds. Reached 43.1 km. Probe crashed without parachute..

1989 November 4 - . 07:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: KRENKEL'. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 60 km (37 mi).

1991 November 4 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 737. LV Family: Trident. Launch Vehicle: Trident D-5.
  • DASO-8 demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1992 November 4 - .
  • Russian Parliament approves START treaty - . Nation: Russia.

1992 November 4 - . 02:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 3. FAILURE: Failure.
  • FOT GT150GM Follow-on Test launch - . Nation: USA. Agency: USAF ACC. Apogee: 100 km (60 mi).

1993 November 4 - . 07:07 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 7. LV Configuration: Skylark 7 MASER 6.
  • MASER 6 Microgravity mission - . Nation: Sweden. Agency: SSC. Apogee: 243 km (150 mi).

1994 November 4 - . 05:47 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2.
  • Resurs-O1 No. 3 - . Payload: Resurs-O1 No. 3. Mass: 1,900 kg (4,100 lb). Nation: Russia. Agency: RAKA. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs-O1. USAF Sat Cat: 23342 . COSPAR: 1994-074A. Apogee: 663 km (411 mi). Perigee: 660 km (410 mi). Inclination: 98.0300 deg. Period: 97.98 min. Studied natural resources. It carried the German Safir-R1 communications experiment as a secondary attached payload. Expected life 3 to 5 years. The spacecraft mass of 1,907 kg was slightly higher than earlier models. The principal Earth observation sensors were MSU-SK and MSU-E instruments along with an experimental PVM-E local vertical sensor .

1994 November 4 - .
  • Landing of Soyuz TM-19 - . Return Crew: Malenchenko; Merbold; Musabayev. Nation: Russia. Related Persons: Malenchenko; Merbold; Musabayev. Program: Mir. Flight: Mir Euromir 94; Mir EO-16; Mir EO-17; Mir LD-4. Soyuz TM-19 undocked from Mir with the crew of Malenchenko, Merbold and Musabayev aboard at 07:29 GMT on November 4. The Soyuz instrument module (PAO, priborno-agregatniy otsek) fired its deorbit engine, and was jettisoned together with the orbital module (BO, bitovoy otsek) at 10:51 GMT, with entry interface for the descent module (SA, spuskaemiy apparat) at 10:54. It landed 170 km north-east of Arkalyk in Kazakhstan on 1994 November 4 at 11:18 GMT.

1995 November 4 - . 14:22 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Delta 7920-X. LV Configuration: Delta 7920-10 D229.
  • Radarsat - . Mass: 2,713 kg (5,981 lb). Nation: Canada. Agency: CSA. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Radarsat. USAF Sat Cat: 23710 . COSPAR: 1995-059A. Apogee: 793 km (492 mi). Perigee: 791 km (491 mi). Inclination: 98.6000 deg. Period: 100.70 min. Summary: Earth imaging with synthetic aperture radar..
  • SURFSAT - . Payload: SURFSAT/Delta 229. Mass: 55 kg (121 lb). Nation: USA. Agency: MDAC. Class: Technology. Type: Navigation technology satellite. Spacecraft: SURFSAT-1. USAF Sat Cat: 23711 . COSPAR: 1995-059B. Apogee: 1,494 km (928 mi). Perigee: 934 km (580 mi). Inclination: 100.6000 deg. Period: 109.70 min. Summary: Test satellite for NASA's Deep Space Network..

1996 November 4 - .
  • Galileo, Callisto 3 Flyby - . Nation: USA. Spacecraft: Galileo.

1996 November 4 - . 17:08 GMT - . Launch Site: Wallops Island DZ. Launch Pad: 37.0 N x 72.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL. LV Configuration: Pegasus XL F14. FAILURE: The rocket functioned perfectly but the separation system failed to release the payload.. Failed Stage: P.
  • HETE - . Nation: USA. Agency: NASA Greenbelt. Program: STEDI. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: HETE. Decay Date: 2002-04-07 . USAF Sat Cat: 24645 . COSPAR: 1996-061A. Apogee: 555 km (344 mi). Perigee: 487 km (302 mi). Inclination: 38.0000 deg. Period: 95.00 min. The High Energy Transient Experiment (HETE) was an international mission led by The Massachusetts Institute of Technology (MIT). Its prime objective was to carry out the first multiwavelength study of gamma ray bursts (GRBs) with UV, X-ray, and gamma ray instruments. A unique feature of the mission was its capability to localise bursts with several arcsecond accuracy, in near real-time aboard the spacecraft. These positions were to be transmitted to the ground, and picked up by a global network of primary and secondary ground stations (SGS), enabling sensitive follow-up studies. However the satellite was never released from its payload fitting. Although signals were received, the solar panels could not deploy, and it went silent after a few days when its batteries ran down.
  • SAC-B - . Nation: Argentina. Agency: CONAE. Program: SAC. Class: Technology. Type: Navigation technology satellite. Spacecraft: SAC-B. Decay Date: 2002-04-07 . USAF Sat Cat: 24645 . COSPAR: 1996-061A. Apogee: 555 km (344 mi). Perigee: 487 km (302 mi). Inclination: 38.0000 deg. Period: 95.00 min.

1998 November 4 - . 05:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 395-02.
  • Panamsat 8 - . Payload: PAS 8. Nation: USA. Agency: Panamsat. Manufacturer: Palo Alto. Program: Panamsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 25522 . COSPAR: 1998-065A. Apogee: 35,810 km (22,250 mi). Perigee: 35,763 km (22,222 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. The Proton launch vehicles Block DM3 fourth stage put the Panamsat PAS 8 into a 6784 km x 35941 km x 17.3 degree transfer orbit. PAS 8 had 24 C-band and 24 Ku-band transponders and was to be located over the Pacific after its R-4D apogee engine manoeuvred the orbit to geostationary altitude and inclination. Geostationary at 166.1 degrees E. Positioned in geosynchronous orbit at 166 deg E in 1998-1999 As of 4 September 2001 located at 166.05 deg E drifting at 0.003 deg W per day. As of 2007 Mar 9 located at 165.96E drifting at 0.002E degrees per day.

1999 November 4 - .
  • ISS Status Report: ISS 99-43 - . Nation: USA. Program: ISS. Summary: Routine operations continue aboard the International Space Station this week as flight controllers monitored systems and made the usual checks of its orientation and spin rate.. Additional Details: ISS Status Report: ISS 99-43.

2000 November 4 - . Launch Site: Taiyuan. LV Family: DF-31. Launch Vehicle: DF-31.
  • Test mission - . Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi).

2001 November 4 - .
2005 November 4 - .
  • International Space Station Status Report: SS05-054 - . Nation: USA. Related Persons: Tokarev; McArthur. Program: ISS. Flight: ISS EO-12. Summary: The Expedition 12 crew prepared for its first spacewalk and kept the international space station ship-shape this week as they passed a milestone of five years of human presence aboard the complex.. Additional Details: International Space Station Status Report: SS05-054.

2006 November 4 - . 13:53 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC6. LV Family: Delta IV. Launch Vehicle: Delta IV Medium. LV Configuration: Delta 4M D4-7 (320) 4040.
  • DMSP-Block-5D3-F17 - . Mass: 1,154 kg (2,544 lb). Nation: USA. Agency: USAF. Program: DMSP. Class: Earth. Type: Weather satellite. Spacecraft: DMSP Block 5D-3. USAF Sat Cat: 29522 . COSPAR: 2006-050A. Apogee: 855 km (531 mi). Perigee: 841 km (522 mi). Inclination: 98.8000 deg. Period: 101.90 min. Defense Meteorological Satellite Program satellite with the Operational Linescan System camera, a microwave imager-sounder, ultraviolet spectrometers, particle detectors, a magnetometer, and a laser threat warning sensor. Reportedly went for a time into safe mode due to software problems after launch. The booster upper stage was conducted a maneuver to deorbit itself after placing the satellite in orbit. After the burn an explosion evidently occurred aboard the stage - dozens of objects were tracked in various orbits with perigees down to 670 km and apogees up to 851 km.

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