Encyclopedia Astronautica
October 31


October 31 Chronology


1902 October 31 - .
  • Birth of Holger N Toftoy - . Nation: USA. Summary: American Army officer, expert in ordnance, responsible for transferring von Braun's rocket technology to the US in 1945. Commanded Huntsville 1954-1956. Held other rockt development posts until retirement in 1960..

1930 October 31 - .
  • Birth of Michael 'Mike' Collins - . Nation: Italy; USA. Summary: American test pilot astronaut. Flew on Gemini 10, Apollo 11. First space walk from one spacecraft to another..

1936 October 31 - .
  • Birth of Sergei Nikolayevich Gaidukov - . Nation: Russia. Summary: Russian navigator cosmonaut, 1967-1978. Retired due to medical reasons (injured during parachute training). Worked as an engineer until 1988, when he retired from all work for medical reasons..

1944 October 31 - . Launch Site: V-2 Battery 444. LV Family: V-2. Launch Vehicle: V-2. FAILURE: Failure.
  • October V-2 results. - . Nation: Germany. Summary: In October, in total the Sonderkommando’s Battery 485 and Battery 444 launched 83 rockets of which 5 failed..

1945 October 31 - . LV Family: Atlas; Mace; Matador; Navaho; Snark. Launch Vehicle: Rascal.
  • US Strategic Missile Programs Begin - . Nation: USA. Program: Navaho. Request For Proposals were issued to 17 contractors by the US Army Air Force for studies of a 10-year R&D program of four missile types. The missiles were to be air-, rail-, road-, or ship- transportable, and fit in three range categories: 280 to 800 km; 800 to 2400 km; and 2400 to 8000 km. Minimum speed was 970 kph, requiring turbojet, ramjet, or rocket propulsion.

1947 October 31 - .
  • XS-1 Flight 55 - . Crew: Yeager. Payload: XS-1 # 1 flight 35. Nation: USA. Related Persons: Yeager. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF flight 13..

1947 October 31 - . 13:41 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: V-2. Launch Vehicle: A-4. LV Configuration: A-4 06T. FAILURE: Loss of control on longitudinal axis..
  • Soviet V-2 launch - . Nation: USSR. Agency: Korolev. Apogee: 0 km ( mi). Summary: Range achieved 2 km..

1949 October 31 - .
1951 October 31 - . LV Family: Redstone. Launch Vehicle: Redstone.
  • Hermes project transferred to Redstone Arsenal. - . Nation: USA. Related Persons: von Braun. Summary: Responsibility for Hermes II transferred to Army Ordnance Guided Missile Center at Redstone Arsenal; Hermes II redesignated the RVA-A-3 test vehicle..

1952 October 31 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Double Deacon. FAILURE: Failure.
  • Navaho Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1956 October 31 - . Launch Site: Sea-launched. Launch Pad: BELA. Launch Platform: B-67. LV Family: R-11. Launch Vehicle: R-11FM.
  • Test mission - . Nation: USSR. Agency: Korolev. Apogee: 150 km (90 mi).

1956 October 31 - . Launch Site: Sea-launched. Launch Pad: BELA. Launch Platform: B-67. LV Family: R-11. Launch Vehicle: R-11FM.
  • Test mission - . Nation: USSR. Agency: Korolev. Apogee: 150 km (90 mi).

1956 October 31 - . 02:04 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC6. LV Family: Redstone. Launch Vehicle: Jupiter A. LV Configuration: Jupiter A RS-25. FAILURE: Malfunction of yaw gyro at approximately 10 sec. Ground cut-off command given.. Failed Stage: G.
  • Jupiter A - . Nation: USA. Agency: USA. Apogee: 0 km ( mi). RS-25 was launched at 2104 hours EST from AMR. The flight was not successful. The behaviour of the missile appeared normal for the first 13 seconds, an early roll disturbance having been smoothly eliminated. Starting at 13 seconds after range zero, the gyro yaw signal indicated increasing yaw for a few seconds and the tracking devices at the same time showed increased displacement to the left of the standard trajectory. The malfunction apparently occurred between the yaw gyro potentiometer output and the outputs of the yaw amplifier of the mixing computer. The primary test objective was to test power plant performance. Missed aimpoint by 264,900 m.

1957 October 31 - . 00:29 GMT - . Launch Site: Pacific Ocean. Launch Pad: 60.7 S x 176.6 W. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon SUI 96.
  • II5.72F Aeronomy / Chemical release mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

1957 October 31 - . 04:52 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC6. LV Family: Redstone. Launch Vehicle: Jupiter A. LV Configuration: Jupiter A CC-41. FAILURE: Loss of inter-compartment pressure at 68 sec. Ground cut-off command given.. Failed Stage: 1.
  • Jupiter A - . Nation: USA. Agency: USA. Apogee: 40 km (24 mi). Launched at 2352 hours EST from AMR. The flight was unsuccessful. Actual range was 48 nm, whereas the predicted range wee 130.588 nm. At 68 seconds, a disturbance occurred in the lateral accelerometer and computer systems. Erroneous guidance instructions were transmitted to the control systems, causing a sharp yaw at 70 seconds. Cut-off was initiated at 98.1 seconds. One of the objectives was to indoctrinate troops for participation in the tactical portions of the countdown. Missed aimpoint by 151,000 m.

1957 October 31 - . 19:51 GMT - . Launch Site: Pacific Ocean. Launch Pad: 65.1 S x 177.9 W. Launch Platform: AGB-4. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon SUI 97.
  • II5.73F Aeronomy / Fields mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

1958 October 31 - . Launch Site: Kheysa. LV Family: R-11. Launch Vehicle: R-11A.
  • First R-11A? Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 103 km (64 mi).

1958 October 31 - . 11:54 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5A.
  • Infrared atmosphere Ionosphere / solar / biology mission - . Nation: USSR. Agency: AN. Apogee: 410 km (250 mi). Summary: Carried dogs to 415 km altitude..

1958 October 31 - . 19:59 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee Hi. LV Configuration: Aerobee Hi NN3.15F.
  • Aeronomy mission - . Nation: USA. Agency: NRL. Apogee: 188 km (116 mi).

1958 October 31 - . 20:46 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun OB6.11.
  • Arctic cloud cover Meteorological / imaging mission - . Nation: USA. Agency: USAF. Apogee: 119 km (73 mi).

1959 October 31 - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: R-7.
  • First R-7 missiles go on alert at Plesetsk. - . Nation: USSR.

1960 October 31 - .
  • Status of qualification and reliability activities for Project Mercury. - . Nation: USA. Program: Mercury. Summary: Space Task Group officials presented the status of qualification and reliability activities for Project Mercury to Dr. T. Keith Glennan, NASA Administrator..

1961 October 31 - . LV Family: Kosmos 3. Launch Vehicle: Kosmos 65S3.
  • Kosmos 65S3 intermediate launch vehicle development authorised. - . Nation: USSR. Spacecraft: Meteor; Strela-1; Strela-2. Summary: Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On the Creation of the Space Carrier 65S3--start of work on a launch vehicle based on the R-14 for launch of the Meteor, Strela, and Pchela satellites.' was issued..

1961 October 31 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: Kosmos 2. Launch Vehicle: R-12.
  • First launch of R-12U from silo. - . Nation: USSR. Agency: MVS. Apogee: 402 km (249 mi).

1962 October 31 - .
  • NAA completed the firm-cost proposal for the definitive Apollo program - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Summary: NAA completed the firm-cost proposal for the definitive Apollo program and submitted it to NASA. MSC had reviewed the contract package and negotiated a program plan position with NAA..

1962 October 31 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • Contract for the S-IVB stage for use in the Saturn C- 1B - . Nation: USA. Program: Apollo. Summary: NASA announced that the Douglas Aircraft Company had been awarded a $2.25million contract to modify the S-IVB stage for use in the Saturn C- 1B program..

1962 October 31 - . 08:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Thor Able-Star. LV Configuration: Thor Ablestar 319 AB012.
  • Anna 1B - . Mass: 161 kg (354 lb). Nation: USA. Agency: USN. Class: Earth. Type: Geodetic satellite. Spacecraft: Anna. USAF Sat Cat: 446 . COSPAR: 1962-B-Mu-1. Apogee: 1,181 km (733 mi). Perigee: 1,075 km (667 mi). Inclination: 50.1000 deg. Period: 107.90 min. Summary: Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

1962 October 31 - . 23:33 GMT - . Launch Site: Eglin. LV Family: Honest John. Launch Vehicle: HJ Nike. LV Configuration: HJ Nike AC20.461. FAILURE: Failure.
  • Firefly III HAZEL Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).

1963 October 31 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • First production F-1 engine delivered - . Nation: USA. Program: Apollo. Summary: The first production F-1 engine for the Apollo Saturn V was flown from Rocketdyne's Canoga Park, Calif., facility, where it was manufactured, to MSFC aboard Aero Spacelines' "Pregnant Guppy.".

1963 October 31 - .
  • The highest leadership of the Soviet Union is busy making the Nikolayev/Tereshkova wedding arrangements. - . Nation: USSR. Related Persons: Nikolayev; Tereshkova. Summary: The highest leadership of the Soviet Union is busy making the Nikolayev/Tereshkova wedding arrangements. Tereshkova disappears for four hours during the day and doesn't show up for important meetings. .

1963 October 31 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 664.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1963 October 31 - . 16:50 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA1. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.94II.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 187 km (116 mi).

1963 October 31 - . 18:00 GMT - . Launch Site: Eglin. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun AC6.341.
  • D-region composition Ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 112 km (69 mi).

1963 October 31 - . 21:17 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA2. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.111GT.
  • Vibration test - . Nation: USA. Agency: NASA. Apogee: 134 km (83 mi).

1964 October 31 - .
  • Death of Theodore Cordy 'Ted' Freeman at Ellington AFB, Texas. Crash of T-38 trainer after bird strike on windshield. - . Nation: USA. Related Persons: Freeman. Summary: American test pilot astronaut, 1963-1964..

1964 October 31 - .
  • Astronaut Theodore C Freeman died in an aircraft accident - . Nation: USA. Related Persons: Freeman. Program: Apollo. Astronaut Theodore C. Freeman died in an aircraft accident at Ellington Air Force Base, near Houston. Freeman, an Air Force captain and a member of NASA's third group of spacemen, was preparing to land his T-38 training jet when it struck a goose and lost power. He ejected from his aircraft, but did not have sufficient altitude for his parachute to open. Freeman thus became the first American astronaut to lose his life in the quest for the moon.

1964 October 31 - . LV Family: UR-700. Launch Vehicle: UR-700.
  • UR-700 project cancelled - . Nation: USSR. Related Persons: Chelomei; Korolev. Program: Lunar L3. Class: Moon. Type: Manned lunar spacecraft. Spacecraft: LK-700. Following the August decree that gave the circumlunar project to Chelomei and the lunar landing project to Korolev, further work on development of the UR-700 by Chelomei was cancelled. However development of the RD-270 engine was continued and Chelomei continued to do UR-700 design studies.

1964 October 31 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 633. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-72.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 October 31 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 599. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-397.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 October 31 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 599. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-450.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 October 31 - . 05:04 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-1. LV Configuration: Mu-1 M-1-1.
  • Test mission - . Nation: Japan. Agency: ISAS. Apogee: 34 km (21 mi).

1967 October 31 - .
  • Cosmos 186 landing. - . Nation: USSR. Related Persons: Rudenko; Ustinov; Mishin. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Due to failure of a star tracker a guided lifting re-entry of 3-4 G was not accomplished. A ballistic re-entry of 7-8 G however resulted in a successful soft landing in the target zone. Rudenko's recovery crews demonstrated a lack of training. Ustinov and Mishin were anxious to release a proclamation of total mission success, but they needed confirmation that the soft landing rockets had functioned correctly. It was only after 2.5 hours that the recovery teams arrived aboard an Mi-6 helicopter that the correct function of the landing system is verified and the leadership notified.

1967 October 31 - . 13:14 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Redstone. Launch Vehicle: Sparta. LV Configuration: SPARTA 2041/SV-9.
  • Sparta SV-9 re-entry vehicle test flight - . Nation: USA. Agency: USA. Apogee: 111 km (68 mi).

1968 October 31 - .
  • Soyuz 3 post-flight debriefing - . Nation: USSR. Related Persons: Beregovoi. Program: Soyuz; Lunar L1. Flight: Soyuz 3. Spacecraft: Soyuz 7K-OK. The post-flight debriefing of Beregovoi reveals that the automated docking sequence from 11,000 to 200 m range from the Soyuz 2 target was normal. At 200 m Beregovoi took over manual control of the spacecraft. At a range of 30 to 40 m he observed the running lights on Soyuz 2 were inverted. He stopped his approach and waited until the spacecraft moved into daylight. By that time the spacecraft were still 30 to 40 m away, but had drifted so that he was 30 degrees off-angle from Soyuz 2. It was in attempting to bring the spacecraft back on axis that he used 30 kg of propellant. He then gave up and hand-flew the spacecraft around Soyuz 2 to take photographs. On the first day of his flight he constantly felt like he was hanging upside-down. This feeling only disappeared on the last day of the flight.

1968 October 31 - .
  • AS-504 and AS-505 missions officially designated as Apollo 9 and Apollo 10 - . Nation: USA. Related Persons: Phillips, Samuel. Program: Apollo. Flight: Apollo 9; Apollo 10. Summary: NASA Apollo Program Director Samuel C. Phillips officially designated the AS-504 and AS-505 missions as Apollo 9 and Apollo 10..

1968 October 31 - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 251 - . Payload: Zenit-4M no. 1. Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4M. Duration: 18.00 days. Decay Date: 1968-11-18 . USAF Sat Cat: 3528 . COSPAR: 1968-096A. Apogee: 255 km (158 mi). Perigee: 201 km (124 mi). Inclination: 64.9000 deg. Period: 89.00 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; deployed radio astronony and gamma ray experiment capsule; maneuverable..

1968 October 31 - . 20:56 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 3. LV Configuration: Black Brant III ADF-3-31.
  • PCA Ionos Aeronomy / ionosphere mission - . Nation: Canada. Agency: NRCC. Apogee: 140 km (80 mi).

1969 October 31 - .
  • Cosmonaut centre starved of equipment. - . Nation: USSR. Summary: Kamanin reviews the scandalous state of equipment deliveries to the cosmonaut centre. Only 10% of the equipment required by party decrees has been delivered, due to lack of support for manned spaceflight by the VVS..

1969 October 31 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-304.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 October 31 - . LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton 8K82K.
  • Soyuz 7K-L1 s/n 10L and 15L - . Payload: Soyuz 7K-L1 s/n 10L and 15L. Nation: USSR. Program: Lunar L1. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-L1. Summary: Despite decision to cancel immediate manned circumlunar flights after Apollo 8, the remaining two L-1 spacecraft were kept in reserve for support of the L3 lunar landing program and possible later manned flights. They were never used..

1970 October 31 - . 10:32 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.41GG-UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1972 October 31 - . 02:42 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission? - . Nation: USSR. Agency: AN. Apogee: 165 km (102 mi).

1972 October 31 - . 10:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission? - . Nation: USSR. Agency: AN. Apogee: 120 km (70 mi).

1972 October 31 - . 13:29 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 527 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MK. Duration: 13.00 days. Decay Date: 1972-11-13 . USAF Sat Cat: 6260 . COSPAR: 1972-086A. Apogee: 306 km (190 mi). Perigee: 207 km (128 mi). Inclination: 65.4000 deg. Period: 89.60 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1972 October 31 - . 23:32 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.106-1.
  • Release Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 170 km (100 mi).

1972 October 31 - . 23:51 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.105-6.
  • Release Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 192 km (119 mi).

1973 October 31 - . 18:24 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 605 - . Payload: Bion no. 1. Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Biology. Type: Biology satellite. Spacecraft: Bion. Duration: 21.50 days. Decay Date: 1973-11-22 . USAF Sat Cat: 6913 . COSPAR: 1973-083A. Apogee: 403 km (250 mi). Perigee: 213 km (132 mi). Inclination: 62.8000 deg. Period: 90.70 min. Summary: Investigation of the influence of space flight on living organisms and testing of life-support systems for biological entities. Capsule recovered 53 deg 29 min N, 65 deg 27 min E..

1974 October 31 - . 10:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53721-253.
  • Intercosmos 12 - . Payload: DS-U2-IK s/n 4. Mass: 400 kg (880 lb). Nation: USSR. Agency: IK. Program: DS. Class: Earth. Type: Ionosphere satellite. Spacecraft: DS-U2-IK. Completed Operations Date: 1975-02-20 . Decay Date: 1975-07-11 . USAF Sat Cat: 7500 . COSPAR: 1974-086A. Apogee: 707 km (439 mi). Perigee: 243 km (150 mi). Inclination: 74.0000 deg. Period: 94.10 min. Summary: Atmospheric, ionospheric research. Comprehensive investigation of the earth's atmosphere and ionosphere and of micrometeorite fluxes..

1975 October 31 - .
  • Enterprise lower fuselage complete. - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Lower forward fuselage on dock, Palmdale, Enterprise (OV-101).

1975 October 31 - . 11:17 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere mission - . Nation: USSR. Apogee: 152 km (94 mi).

1976 October 31 - .
  • Solid rocket booster 1/4-scale model - . Nation: USA. Program: STS. Summary: Solid rocket booster 1/4-scale model (burnout configuration).

1977 October 31 - . Launch Site: Baikonur. LV Family: R-36M. Launch Vehicle: R-36MU 15A18.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 October 31 - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Taurus Tomahawk. LV Configuration: Taurus Tomahawk NASA 12.1005WT.
  • Test mission - . Nation: USA. Agency: NASA. Apogee: 554 km (344 mi).

1979 October 31 - . 09:25 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Vostok 8A92M.
  • Meteor 2-05 - . Payload: Meteor-2 no. 5. Mass: 2,750 kg (6,060 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Weather satellite. Spacecraft: Meteor-2. USAF Sat Cat: 11605 . COSPAR: 1979-095A. Apogee: 881 km (547 mi). Perigee: 862 km (535 mi). Inclination: 81.2000 deg. Period: 102.40 min. Summary: Acquisition of meteorological information required for use in the operational weather service with the aid of advanced equipment. .

1980 October 31 - . 03:54 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur SLV-3D. LV Configuration: SLV-3D Centaur AC-57 / Centaur D-1AR 5037.
  • Fltsatcom 4 - . Mass: 1,800 kg (3,900 lb). Nation: USA. Agency: USN. Class: Communications. Type: Military communications satellite. Spacecraft: Fltsatcom. USAF Sat Cat: 12046 . COSPAR: 1980-087A. Apogee: 35,803 km (22,246 mi). Perigee: 35,769 km (22,225 mi). Inclination: 9.2000 deg. Period: 1,436.10 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 171 deg E from 1981. Last known longitude (25 July 1999) 172.61 deg E drifting at 0.001 deg W per day.

1980 October 31 - . 12:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1219 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-6U. Duration: 13.00 days. Decay Date: 1980-11-13 . USAF Sat Cat: 12050 . COSPAR: 1980-088A. Apogee: 312 km (193 mi). Perigee: 189 km (117 mi). Inclination: 72.9000 deg. Period: 89.50 min. Summary: Photo surveillance; returned film capsule; maneuverable..

1981 October 31 - . 09:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 3C. LV Configuration: Titan IIIC 23C-21 (3C-39).
  • Chalet 3 - . Payload: Chalet 3 (Vortex 3) / OPS 4029. Mass: 820 kg (1,800 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Chalet. USAF Sat Cat: 12930 . COSPAR: 1981-107A. Apogee: 382 km (237 mi). Perigee: 134 km (83 mi). Inclination: 29.3000 deg. Period: 90.40 min. Summary: Chalet ELINT satellite..

1981 October 31 - . 22:54 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Cosmos 1317 - . Payload: Oko #23. Mass: 1,250 kg (2,750 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. USAF Sat Cat: 12933 . COSPAR: 1981-108A. Apogee: 34,987 km (21,739 mi). Perigee: 5,425 km (3,370 mi). Inclination: 68.3000 deg. Period: 719.00 min. Summary: Covered Oko constellation plane 8 - 196 degree longitude of ascending node..

1982 October 31 - . 11:20 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Progress 16 - . Payload: Progress s/n 115. Mass: 7,020 kg (15,470 lb). Nation: USSR. Agency: MOM. Program: Salyut 7. Class: Manned. Type: Manned logistics spacecraft. Flight: Salyut 7 EO-1. Spacecraft: Progress. Duration: 44.25 days. Completed Operations Date: 1982-12-14 17:16:24 . Decay Date: 1982-12-14 17:16:24 . USAF Sat Cat: 13638 . COSPAR: 1982-107A. Apogee: 246 km (152 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg. Period: 88.80 min. Summary: Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 2 Nov 1982 13:22:00 GMT. Undocked on 13 Dec 1982 15:32:00 GMT. Destroyed in reentry on 14 Dec 1982 17:17:00 GMT. Total free-flight time 3.16 days. Total docked time 41.09 days..

1983 October 31 - . 20:30 GMT - . Launch Site: Eareckson. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 44 km (27 mi).

1984 October 31 - . 12:29 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 1607 - . Mass: 3,800 kg (8,300 lb). Nation: USSR. Agency: MO. Program: RORSAT. Class: Surveillance. Type: Military naval surveillance radar satellite. Spacecraft: US-A. Decay Date: 1985-03-28 . USAF Sat Cat: 15502 . COSPAR: 1984-112B. Apogee: 994 km (617 mi). Perigee: 908 km (564 mi). Inclination: 65.0000 deg. Period: 104.10 min. Summary: Ocean surveillance; nuclear powered..

1985 October 31 - . 03:59 GMT - . Launch Site: Eareckson. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 55 km (34 mi).

1986 October 31 - . 08:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1789 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs F1-14F40. Duration: 14.00 days. Decay Date: 1986-11-14 . USAF Sat Cat: 17054 . COSPAR: 1986-084A. Apogee: 272 km (169 mi). Perigee: 178 km (110 mi). Inclination: 82.6000 deg. Period: 89.00 min. Summary: Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. .

1989 October 31 - . 17:30 GMT - . Launch Site: Primrose Lake. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1990 October 31 - . 22:14 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 94 km (58 mi).

1992 October 31 - . Launch Site: Alcantara. LV Family: Sonda. Launch Vehicle: Sonda 2. LV Configuration: Sonda 2 XV-56.
  • Ponta de Areia Ionosphere mission - . Nation: Brazil. Agency: INPE; IAE. Apogee: 32 km (19 mi).

1993 October 31 - .
1994 October 31 - . 14:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 361-02.
  • Elektro 1 - . Payload: Elektro s/n 1L. Mass: 2,850 kg (6,280 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Weather satellite. Spacecraft: Elektro . Completed Operations Date: 1998-09-01 . USAF Sat Cat: 23327 . COSPAR: 1994-069A. Apogee: 35,799 km (22,244 mi). Perigee: 35,782 km (22,233 mi). Inclination: 4.7000 deg. Period: 1,436.30 min. Stationed at 76.61 deg E. Elektro 1 was finally launched on 31 October 1994, 15 years after its original public schedule. Malfunction of the local vertical sensor and the attitude control system delayed the positioning of the spacecraft at its intended location of 76 degrees E, but by early December Elektro 1 was on station. However problems with the local vertical sensor continued to plague the spacecraft, and useful images were not available. Stayed in geosynchronous orbit at 76 deg E in 1995-1998 before being shut down. As of 4 September 2001 located at 71.89 deg E drifting at 0.069 deg E per day. As of 2007 Mar 10 located at 67.89E drifting at 0.000W degrees per day.

1995 October 31 - . 20:19 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2.
  • Cosmos 2322 - . Payload: Tselina-2 no. 19. Mass: 6,000 kg (13,200 lb). Nation: Russia. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-2. USAF Sat Cat: 23704 . COSPAR: 1995-058A. Apogee: 854 km (530 mi). Perigee: 847 km (526 mi). Inclination: 71.0000 deg. Period: 102.00 min.

1997 October 31 - .
  • Mir News 392: Results 3d spacewalk (IVA) 24d Main Expedition Mir - . Nation: Russia. Program: Mir. Flight: Mir NASA-5; Mir EO-24. On 24.10.97 the cables from the vacuum plate to the solar panel interface in the Kristall module had been deployed and after some tests 2 of the 3 still living panels on the Spektr could be turned to the most effective angle towards the sun. Already on 25.10 Solovyov got the first series of instructions for the next 2 spacewalks, EVA's this time, on 3 and 6.11.97. From this day on practically all activities were related to those operations.

    On 26.10 Solovyov reported enormous forest fires in the area of Barnaul (Siberia). The crew had discovered the fire already the day before, but now these fires had considerably increased. Along a front of 100 KM the fire moved to the North-West. Solovyov wondered why the media did not give any information about these fires. As of Monday, 27.10, the preparations for the 1st EVA on 3.11.97 began. The crew got comprehensive instructions, i.e. a video-simulation of the operation and a huge amount of documentation.

    During the following days they collected and took stock off the equipment needed for the spacewalk and they replaced goods from the airlock and the scientific- and instrument compartment of the Kvant-2 module to other locations in the complex. The crew checked the 2 Orlan M suits and the communication systems during the EVA. On Friday, 31.10, these preparations were concluded during a long communications session via Altair-2 in which TsUP transmitted video images of the areas in which the cosmonauts have to work during the EVA. These areas cannot be fully seen via the portholes of the complex.

    During this video session the cosmonauts asked a lot of questions and got additional instructions. The crew also downlinked images of one of the solar panels which did not regularly turn. It sometimes stopped and went on stuttering (Thus far I do not know which panel.)

    During radio traffic in orb. 66833 (0918-0926 UTC) the crew spoke with Sergey Samburov, RV3DR, grandson of the famous rocket pioneer Tsiolkovskiy, about the minisputnik PS-2 (also named Sputnik 40 and RS-17), which will be launched by Vinogradov during the EVA on 3.11. The cosmonauts had already checked the transmitters and heard the Blieb Blieb signals. Samburov, the radio-amateur mentor of all cosmonauts, urged them not to forget to switch on the transmitters before deploying the satellite. They have to do that after donning of the spacesuits.

    The EVA's:

    On 3.11.97, from 0130 UTC (opening hatch) until appr. 0700 UTC. On 6.11.97, from 0030 UTC until appr. 0600 UTC. Don't forget to monitor 145.820 and 145.840 mc for the Sputnik ' Bliebs' during Mir's passes in the morning of 3.11.97.

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


1998 October 31 - .
  • STS-95 Mission Status Report # 05 - . Nation: USA. Related Persons: Brown; Duque; Glenn; Mukai; Parazynski. Program: STS. Flight: STS-95. Summary: Medical investigations will begin in earnest today as Discovery's crew moves forward with research comparing the changes the human body goes through when making trips into orbit with the changes that occur as part of the natural aging process on Earth.. Additional Details: STS-95 Mission Status Report # 05.

2000 October 31 - . 07:52 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U A15000-666.
  • Soyuz TM-31 - . Call Sign: Uran. Crew: Gidzenko; Krikalyov; Shepherd. Payload: Soyuz TM 11F732 s/n 205. Mass: 7,250 kg (15,980 lb). Nation: Russia. Related Persons: Gidzenko; Krikalyov; Shepherd. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EO-1. Spacecraft: Soyuz TM. Duration: 186.91 days. Decay Date: 2001-05-06 . USAF Sat Cat: 26603 . COSPAR: 2000-070A. Apogee: 385 km (239 mi). Perigee: 378 km (234 mi). Inclination: 51.5000 deg. Period: 92.18 min. Soyuz TM-31 delivered the Expedition One crew to the International Space Station with Gidzenko as the Soyuz crew commander with the call-sign 'Uran'. The spacecraft docked at Zvezda's rear port at 0921 GMT on November 2. The hatch to Zvezda was opened at 1023 GMT. Once aboard ISS, Shepherd became the ISS Commander, with 'Station Alpha' as the ISS callsign. Soyuz TM-31, with Shepherd, Gidzenko and Krikalyov aboard, undocked from the -Y port on Zvezda on February 24, 2001 at 1006 GMT and redocked with the -Z port on Zarya at 1037 GMT. This freed the Zvezda port for a Progress resupply ship. After the departure of the Progress, Soyuz TM-31 undocked from the Zarya nadir port April 18 2001 at 1240 GMT and redocked with the Zvezda aft port at 1301 GMT, leaving clearance for the Raffaello MPLM module to be berthed at the Unity nadir during the STS-100 mission.

2001 October 31 - .
  • Landing of Soyuz TM-32 - . Return Crew: Afanasyev; Kozeyev; Andre-Deshays. Nation: Russia. Related Persons: Afanasyev; Kozeyev; Andre-Deshays. Program: ISS. Flight: ISS EP-2. The EP-2 crew - Afanasyev, Kozeyev and Andre-Deshays - undocked Soyuz TM-32 from the Pirs module at 01:38:30 GMT on October 31. The deorbit burn was at 04:04 GMT, with landing 180 km southeast of Dzhezkazgan at 04:59:26 GMT. This left the Expedition-3 crew of Culbertston, Dezhurov and Tyurin with Soyuz TM-33, docked with the Zarya module, as the station lifeboat.

2003 October 31 - .
  • International Space Station Status Report #03-57 - . Nation: USA. Related Persons: Duque; Foale; Kaleri; Lu; Malenchenko. Program: ISS. Flight: ISS EO-8. International Space Station Expedition 8 Commander and NASA ISS Science Officer Michael Foale and Flight Engineer Alexander Kaleri wound up their first full workweek in space Friday. Science activities, Station maintenance, exercise and more familiarization with their new home were their focus. Additional Details: International Space Station Status Report #03-57.

2010 October 31 - . 16:26 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3C.
  • Beidou G4 - . Payload: Beidou DW6. Nation: China. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou. USAF Sat Cat: 37210 . COSPAR: 2010-057A. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 1.6000 deg. Period: 1,436.10 min. Summary: Navigation satellite..

2011 October 31 - .
  • Shenzhou 8 - . Nation: China. Spacecraft: Shenzhou. USAF Sat Cat: 37859 . COSPAR: 2011-063A. Apogee: 338 km (210 mi). Perigee: 328 km (203 mi). Inclination: 42.8000 deg. Period: 91.20 min. Summary: Unmanned Shenzhou spacecraft. Automatically docked with Tiangong 1 space laboratory..

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