Encyclopedia Astronautica
November 18


November 18 Chronology


1900 November 18 - .
  • Birth of George B Kistiakowsky - . Nation: USA. Summary: American chemist, associated with the development of the atomic bomb, and later an advocate of banning nuclear weapons..

1923 November 18 - .
  • Birth of Alan Bartlett Jr 'Al' Shepard - . Nation: USA. Summary: American test pilot astronaut. Flew on Mercury MR-3, Apollo 14. First American in space. Grounded due on medical grounds during Gemini, but reinstated, becoming fifth person to walk on the moon. Millionaire entrepreneur on the side., Apollo 14, , , , , ,.

1929 November 18 - .
1939 November 18 - . LV Family: Goddard. Launch Vehicle: Goddard P-C.
  • Goddard Series P Section C rocket tests - . Nation: USA. Related Persons: Goddard. Section C tests would run through October 10, 1941. The series of twenty-four static and flight tests (P13-P36) was made with rockets of large fuel capacity, with the rocket motor, pumps, and turbines previously developed. These rockets averaged nearly 22 ft in length, and were 18 in, in diameter. They weighed empty from 190 to 240 lb. The liquid-oxygen load averaged about 140 lb, the gasoline 112 lb, making 'quarter-ton' loaded rockets.

1944 November 18 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 19544. FAILURE: Failed (impact of rocket with explosion of warhead at ground level).
  • V-2 Ma290 245 N3 - . Nation: Germany. Summary: Planned range 200 km. Failed - accuracy was 4 km to the right of the planned trajectory. Circular error 124.1 km from aim point..

1948 November 18 - .
1948 November 18 - . 22:35 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 44.
  • Hermes B Solar/Biological mission - . Nation: USA. Agency: USA; GE. Apogee: 145 km (90 mi). Launched 15:34 local time. Reached 145.6 km. Carried biological (Harvard), solar radiation (Naval Research Lab), composition (Signal Corps Engineering Lab, University of Michigan) experiments for General Electric. The warhead section was replaced with an instrumented full-scale replica of the cylindrical GE A-4 ramjet duct planned for the Hermes B ramjet missile.

1949 November 18 - . 16:03 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 56.
  • UM Sampling,Grenades Aeronomy / Chemical release mission - . Nation: USA. Agency: USA; UM. Apogee: 124 km (77 mi). Summary: Launched 08:03 local time. Reached 124.2 km. Carried winds, composition, temperature; cosmic radiation (APL, John Hopkins); and solar radiation (Naval Research Lab) experiments for Signal Corps Engineering Lab, University of Michigan..

1951 November 18 - .
  • Birth of Mark Neil Brown - . Nation: USA. Summary: American engineer mission specialist astronaut. Flew on STS-28, STS-48..

1952 November 18 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bechar. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique N8. FAILURE: Failure.
  • Test mission - . Nation: France. Agency: LRBA. Apogee: 0 km ( mi).

1953 November 18 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-11104.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1954 November 18 - . LV Family: Navaho. Launch Vehicle: Navaho.
  • Navaho inertial system tested. - . Nation: USA. Program: Navaho. Summary: Inertial guidance system for Navaho X-10 missile tested in first flight at Downey, California aboard North American's T-39 testbed..

1955 November 18 - .
  • X-2 Flight 5 - . Crew: Everest. Payload: X-2 # 1 flight 5. Nation: USA. Related Persons: Everest. Class: Manned. Type: Manned rocketplane. Spacecraft: X-2 . Summary: First powered flight. Mach 0.992 at 10,675 m. Slight fire damage from engine bay fire..

1958 November 18 - . 04:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas B. LV Configuration: Atlas B 9B.
  • Research and development launch - . Nation: USA. Agency: USAF. Apogee: 800 km (490 mi).

1958 November 18 - . 16:47 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun OB6.14.
  • Arctic cloud cover Meteorological / imaging mission - . Nation: USA. Agency: USAF. Apogee: 116 km (72 mi).

1958 November 18 - . 21:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC9. LV Family: Navaho. Launch Vehicle: Navaho G-26. LV Configuration: Navaho II SM-64 04. FAILURE: Disintegrated at moment of booster shutdown.. Failed Stage: 1.
  • Navaho G-26 Flight 11 RISE-2 - . Nation: USA. Agency: USAF. Apogee: 23 km (14 mi). Summary: The vehicle disintegrated at 23.5 km altitude at the time of booster shutdown and cruse stage separation. The USAF canceled further RISE flights and this definitively marked the end of the Navaho..

1959 November 18 - . 05:03 GMT - . Launch Site: Akita. LV Family: Kappa. Launch Vehicle: Kappa 7. LV Configuration: Kappa 7 K-7-1.
  • Test mission - . Nation: Japan. Agency: ISAS. Apogee: 53 km (32 mi).

1959 November 18 - . 19:30 GMT - . Launch Site: Eglin. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp AA8.241C.
  • Ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 206 km (128 mi).

1959 November 18 - . 22:17 GMT - . Launch Site: Wallops Island. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp NASA 03.15CA.
  • Sodium release Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 250 km (150 mi). Summary: Nike-Asp sounding rocket fired from NASA Wallops Station emitted sodium vapor at 80 km to 250 km altitude, revealing powerful windshear effects..

1960 November 18 - . LV Family: Atlas. Launch Vehicle: Atlas D.
  • Mercury Spacecraft No. 8 delivered to Cape Canaveral - . Nation: USA. Program: Mercury. Spacecraft: Mercury. Summary: Spacecraft No. 8 was delivered to Cape Canaveral for the Mercury-Atlas 3 (MA-3) unmanned orbital mission..

1960 November 18 - . 03:39 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.26GE.
  • SBE 13 Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 128 km (79 mi).

1960 November 18 - . 23:39 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.27GE.
  • SBE 14 Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 129 km (80 mi).

1961 November 18 - . 06:30 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.72NA.
  • Airglow Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 142 km (88 mi).

1961 November 18 - . 08:12 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC12. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 117D (AA2) / Agena B 6002 (AA2). FAILURE: Agena B Second Stage failed to restart.. Failed Stage: 2.
  • Ranger 2 - . Payload: NASA P-33 (RA-2). Mass: 304 kg (670 lb). Nation: USA. Agency: NASA. Program: Ranger. Class: Moon. Type: Lunar probe. Spacecraft: Ranger 1-2. Decay Date: 1961-11-20 . USAF Sat Cat: 206 . COSPAR: 1961-A-Theta-1. Apogee: 242 km (150 mi). Perigee: 150 km (90 mi). Inclination: 33.3000 deg. Period: 88.30 min. This was a flight test of the Ranger spacecraft system designed for future lunar and interplanetary missions. The spacecraft was launched into a low earth parking orbit, but an inoperative roll gyro prevented Agena restart resulting in Ranger 2 being stranded in low earth orbit. The orbit decayed and the spacecraft reentered Earth's atmosphere on 20 November 1961.

1961 November 18 - . 13:42 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LC-A. Launch Vehicle: Journeyman. LV Configuration: Journeyman NASA 11.05GB.
  • BIOS I Biological mission - . Nation: USA. Agency: NASA. Apogee: 1,057 km (656 mi).

1962 November 18 - .
1962 November 18 - . 04:57 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.27NP.
  • LeRC LH2 test Technology test - . Nation: USA. Agency: NASA. Apogee: 206 km (128 mi).

1963 November 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LC-A. LV Family: Honest John. Launch Vehicle: HJ Nike Nike. LV Configuration: HJ Nike Nike HAD-1.
  • LRL HAD-1 test - . Nation: USA. Agency: Livermore. Apogee: 163 km (101 mi).

1964 November 18 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-66.
  • Ballistic Aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 309 km (192 mi).

1964 November 18 - . 11:23 GMT - . Launch Site: Eglin. LV Family: Apache. Launch Vehicle: Nike Apache. FAILURE: Failure.
  • LILA Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 143 km (88 mi).

1964 November 18 - . 20:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Thor Agena D SLV-2A/D. LV Configuration: Thor SLV-2A Agena D 416 / Agena D SS-01A 1180.
  • KH-4A 1014 (ORBIS) - . Payload: KH-4A s/n 1014 & Orbis / Agena D 1180 / OPS 3360. Mass: 1,500 kg (3,300 lb). Nation: USA. Agency: NRO; CIA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-4A. Decay Date: 1964-12-06 . USAF Sat Cat: 930 . COSPAR: 1964-075A. Apogee: 329 km (204 mi). Perigee: 177 km (109 mi). Inclination: 70.0000 deg. Period: 89.60 min. Summary: KH-4A. Cameras operated successfully..
  • ORBIS - . Nation: USA. Agency: USAF. Spacecraft: KH-4A. Decay Date: 1964-12-06 . USAF Sat Cat: 930 . COSPAR: 1964-075xx. Apogee: 276 km (171 mi). Perigee: 167 km (103 mi). Inclination: 70.0000 deg. Period: 88.90 min.

1965 November 18 - . Launch Site: Eglin. LV Family: Javelin. Launch Vehicle: Nike Javelin.
  • IQSY Na, TMA Aeronomy sodium / TMA release mission - . Nation: USA. Agency: AFCRL. Apogee: 130 km (80 mi).

1965 November 18 - . 02:20 GMT - . Launch Site: Eglin. LV Family: Arcas. Launch Vehicle: Sparrow Arcas. LV Configuration: Sparrow Arcas NA-FLORA /S-4.
  • Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 130 km (80 mi).

1965 November 18 - . 05:20 GMT - . Launch Site: Eglin. LV Family: Arcas. Launch Vehicle: Sparrow Arcas. LV Configuration: Sparrow Arcas S-3.
  • Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 130 km (80 mi).

1965 November 18 - . 05:20 GMT - . Launch Site: Eglin. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.382.
  • IQSY D-region comparison Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 116 km (72 mi).

1965 November 18 - . 08:01 GMT - . Launch Site: Eglin. LV Family: Arcas. Launch Vehicle: Sparrow Arcas. LV Configuration: Sparrow Arcas NA-HANNAH /S-6.
  • Aeronomy / ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 137 km (85 mi).

1965 November 18 - . 11:21 GMT - . Launch Site: Eglin. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun CRL AE6.499.
  • POLLY Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 155 km (96 mi).

1965 November 18 - . 14:31 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.78UA.
  • Pandora 1 (Leonids) Meteorites mission - . Nation: USA. Agency: NASA. Apogee: 149 km (92 mi).

1965 November 18 - . 17:45 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bechar. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C119.
  • MPE Ba-14 Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 170 km (100 mi).

1966 November 18 - .
1966 November 18 - . Launch Site: Edwards. Launch Complex: Edwards RW04/22. Launch Platform: NB-52. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3- A-84. FAILURE: Failure.
  • X-15A-2 test - . Nation: USA. Agency: NASA; USAF. Apogee: 14 km (8 mi). Summary: Unofficial world's speed record. Maximum Speed - 6838 kph. Maximum Altitude - 30140 m..

1966 November 18 - . Launch Site: Yuma. LV Family: Martlet. Launch Vehicle: Martlet 2.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 180 km (110 mi). A Martlet 2C launched from the 16 inch L86 gun established the world altitude record for a sub-orbital gun-launched projectile. A Martlet 2C was fired to an altitude of 180 km with a flight time of over 400 seconds. Launched from Yuma Proving Ground, Arizona - Latitude: 32.87 N, Longitude:114.32 W.

1966 November 18 - . 01:05 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 3 AC. LV Configuration: Skylark 3 AC SL481. FAILURE: Failure.
  • Test mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 142 km (88 mi).

1966 November 18 - . 22:15 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.299UA.
  • Meteoroids Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 161 km (100 mi).

1967 November 18 - .
  • L1 launch weather delays. - . Nation: USSR. Related Persons: Mishin. Program: Lunar L1. Summary: Bad weather at Baikonur. Low visibility and snow may delay the L1 launch. Kamanin rails against Mishin - he's a drunk, an authoritarian, etc. etc..

1968 November 18 - .
  • Zond 6 re-entry - . Nation: USSR. Program: Lunar L1. Spacecraft: Soyuz 7K-L1. By 20:00 the cabin pressure was down to 180 mm, and then reached 25 mm at re-entry. At 16:00 the spacecraft confirmed that all landing commands had been received successfully. At 16:20 it confirmed correct orientation for re-entry. The tracking vessel Komarov tracked the capsule in its first dip into the atmosphere over the Indian Ocean. The tracking ship crew estimated the capsule would miss the landing point by 1800 km. However Zond 6 successfully completed the double-skip re-entry. It was picked up by PVO radars 300 km from the border of Afghanistan, and tracked to 100 to 150 km north of the cosmodrome. Radio communications and the radar transponder aboard the capsule were inoperative, and the precise landing point could not be determined. The parachute should have deployed at 17:19 and Kiev and Baku received a brief 1 to 2 second radio burst from the capsule, but nothing thereafter. A search begins for the capsule using 50 aircraft and 12 helicopters. Finally at 06:35 the next morning an Mi-4 sees the parachute 38 km southeast of Novokazalinsk, 70 km from Baikonur. The spacecraft is found 3 km away at 12:00.

1969 November 18 - . 02:17 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 3 AC. LV Configuration: Skylark 3 AC SL602. FAILURE: Failure.
  • Fresnel shadowgraph X-ray astronomy mission - . Nation: UK. Agency: BAC. Apogee: 208 km (129 mi).

1969 November 18 - . 03:47 GMT - .
  • Apollo 12 enters lunar orbit - . Nation: USA. Flight: Apollo 12. At 03:47 GMT November 18 Apollo 12 arrived at the moon 83 1/2 hours after liftoff. Conrad fired the main propulsion engine for almost 6 minutes to go into an elliptical lunar orbit. Five hours later a second burn put the spacecraft into a circular orbit at 60 nautical miles (111 kilometers) altitude, where Yankee Clipper would stay until it was time to return to earth. Additional Details: Apollo 12 enters lunar orbit.

1969 November 18 - . 13:34 GMT - . Launch Site: Biscarosse. LV Family: Belier. Launch Vehicle: Dragon 3. LV Configuration: Dragon 3 D-304.
  • FU-192 Plasma Ionosphere mission - . Nation: France. Agency: CNES. Apogee: 475 km (295 mi).

1969 November 18 - . 21:32 GMT - . Launch Site: Tonopah. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-135.
  • LRL ACS-5 Solar x-ray mission - . Nation: USA. Agency: Sandia. Apogee: 174 km (108 mi).

1970 November 18 - .
  • Luna 17 lands on moon. - . Nation: USSR. Related Persons: Chelomei. Program: Luna. Spacecraft: Luna Ye-8; Lunokhod. Summary: Luna 17 / Lunokhod have landed on the Sea of Storms on the moon. Chelomei is assisting Kamanin in securing funds for the water basin for zero-G training, further simulators, etc..

1970 November 18 - . 12:30 GMT - . Launch Site: Poker Flat. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.93UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1970 November 18 - . 21:29 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Delta. Launch Vehicle: Thorad Agena D SLV-2H. LV Configuration: Thorad SLV-2H Agena D 552 / Agena D 1658.
  • KH-4B 1112 - . Payload: KH-4B s/n 1112 / Agena D 1658 / OPS 4992. Mass: 2,000 kg (4,400 lb). Nation: USA. Agency: NRO; CIA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-4B. Decay Date: 1970-12-11 . USAF Sat Cat: 4721 . COSPAR: 1970-098A. Apogee: 227 km (141 mi). Perigee: 180 km (110 mi). Inclination: 82.9000 deg. Period: 88.50 min. Summary: KH-4B. The forward camera failed on pass 104 and remained inoperative throughout the rest of the mission..
  • OPS 6829 - . Payload: EHH B20. Nation: USA. Agency: USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1977-09-14 . USAF Sat Cat: 4722 . COSPAR: 1970-098xx. Apogee: 206 km (128 mi). Perigee: 195 km (121 mi). Inclination: 83.2000 deg. Period: 88.50 min.
  • SRV 827 - . Payload: SRV 1112-1 / OPS 6829. Mass: 60 kg (132 lb). Nation: USA. Agency: NRO; USAF. Spacecraft: KH-4B. Decay Date: 1977-09-14 . USAF Sat Cat: 4722 . COSPAR: 1970-098B. Apogee: 505 km (313 mi). Perigee: 493 km (306 mi). Inclination: 83.1000 deg. Period: 94.60 min. Summary: Radar monitoring..

1971 November 18 - . 01:01 GMT - . Launch Site: Sonmiani. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P123S/C.
  • Lithium release Aeronomy mission - . Nation: UK. Agency: SRC. Apogee: 120 km (70 mi).

1971 November 18 - . 07:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • OT GT07GM operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 November 18 - . 07:04 GMT - . Launch Site: Pacific Ocean. Launch Pad: 27.4 N x 125.0 W. Launch Platform: AVM1. LV Family: Sandhawk. Launch Vehicle: Hydra Sandhawk.
  • LRL BOX-17 Test / x-ray astronomy mission - . Nation: USA. Agency: USN NMC. Apogee: 267 km (165 mi). Summary: Launched at Pacific Ocean Launch Site 7 LP1 - - Latitude: 27.38 N - Longitude: 125.00 W..

1972 November 18 - . Launch Site: El Arenosillo. LV Family: Skua. Launch Vehicle: Skua 1.
  • Ionosphere mission - . Nation: USA. Agency: INTA; DLR. Apogee: 94 km (58 mi).

1973 November 18 - . 21:22 GMT - . Launch Site: Natal. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.63UI-II.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 650 km (400 mi).

1973 November 18 - . 23:34 GMT - . Launch Site: CELPA. LV Family: Canopus. Launch Vehicle: Rigel.
  • Ionosphere mission - . Nation: Argentina. Agency: CONAE. Apogee: 250 km (150 mi).

1974 November 18 - . 21:00 GMT - . Launch Site: Poker Flat. Launch Vehicle: Rocketsonde.
  • Met Para, Datasonde - . Nation: USA. Agency: MRN. Apogee: 65 km (40 mi).

1975 November 18 - . 19:01 GMT - . Launch Site: Wallops Island. LV Family: Javelin. Launch Vehicle: Nike Javelin. LV Configuration: Nike Javelin NASA 32.01WT.
  • Test mission - . Nation: USA. Agency: NASA. Apogee: 163 km (101 mi).

1976 November 18 - .
  • Start escape system sled test, Holloman, N.M. - . Nation: USA. Program: STS.

1976 November 18 - . 04:25 GMT - . Launch Site: Thumba. LV Family: Belier. Launch Vehicle: Centaure 2B. LV Configuration: Centaure 2B ISRO 5.37.
  • ISRO 5.37 Ionosphere mission - . Nation: India. Agency: ISRO. Apogee: 128 km (79 mi).

1977 November 18 - . Launch Site: Edwards. LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Fourth ferry flight test, Edwards - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Fourth ferry flight test, Edwards (3 hours, 37 minutes), Enterprise (OV-101).

1980 November 18 - . 16:30 GMT - . Launch Site: ETR Launch Area. Launch Platform: UK S26. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3TK.
  • Chevaline warhead test launch - . Nation: UK. Agency: RN. Apogee: 1,000 km (600 mi).

1981 November 18 - . 14:00 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1982 November 18 - . 09:25 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1421 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-6U. Duration: 14.00 days. Decay Date: 1982-12-02 . USAF Sat Cat: 13661 . COSPAR: 1982-112A. Apogee: 259 km (160 mi). Perigee: 206 km (128 mi). Inclination: 70.3000 deg. Period: 89.20 min. Summary: Photo surveillance; returned film capsule; maneuverable..

1982 November 18 - . 11:20 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton-K 306-02.
  • Iskra 3 - . Payload: RK-03. Nation: USSR. Agency: MOM. Program: Salyut 7. Class: Communications. Type: Amateur radio communications satellite. Flight: Salyut 7 EO-1. Spacecraft: Iskra. Decay Date: 1982-12-16 . USAF Sat Cat: 13663 . COSPAR: 1982-033AD. Apogee: 356 km (221 mi). Perigee: 349 km (216 mi). Inclination: 51.6000 deg. Period: 91.60 min. Summary: Launched from Salyut 7 airlock. Conduct of experiments in the field of amateur radiocommunications. .

1983 November 18 - . 06:32 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Atlas. Launch Vehicle: Atlas E. LV Configuration: Atlas E 58E / Star-37S-ISS.
  • DMSP-Block-5B5D2-2 - . Payload: DMSP S-7 / OPS 1294. Mass: 750 kg (1,650 lb). Nation: USA. Agency: USAF. Program: DMSP. Class: Earth. Type: Weather satellite. Spacecraft: DMSP Block 5D-2. USAF Sat Cat: 14506 . COSPAR: 1983-113A. Apogee: 818 km (508 mi). Perigee: 801 km (497 mi). Inclination: 98.4000 deg. Period: 101.10 min. Summary: Defense Meteorological Satellite Program..

1985 November 18 - . 17:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1986 November 18 - . 14:08 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 334-01.
  • Gorizont 13 - . Payload: Gorizont s/n 22L. Mass: 2,100 kg (4,600 lb). Nation: USSR. Agency: MOM. Class: Communications. Type: Civilian communications satellite. Spacecraft: Gorizont . Completed Operations Date: 1991-04-18 . USAF Sat Cat: 17083 . COSPAR: 1986-090A. Apogee: 36,863 km (22,905 mi). Perigee: 36,759 km (22,840 mi). Inclination: 10.3000 deg. Period: 1,488.80 min. Stationed at 90 deg E. Provision of telephone and telegraph radiocommunications and television broadcasting. Positioned in geosynchronous orbit at 90 deg E in 1986-1991 As of 5 September 2001 located at 132.70 deg W drifting at 12.791 deg W per day. As of 2007 Mar 10 located at 94.81E drifting at 12.778W degrees per day.

1987 November 18 - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Honest John. Launch Vehicle: HJ Nike Hydac.
  • HAVE JEEP VIII-A Reentry test - . Nation: USA. Agency: USAF BMD. Apogee: 500 km (310 mi).

1987 November 18 - . 13:06 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 N. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.023UG.
  • Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).

1988 November 18 - . 00:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 1979 - . 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: 1989-12-25 . USAF Sat Cat: 19647 . COSPAR: 1988-101A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.0000 deg. Period: 92.70 min. Summary: Ocean surveillance..

1989 November 18 - . 14:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Delta 5920-8. LV Configuration: Delta 5920-8 D189.
  • COBE - . Mass: 2,265 kg (4,993 lb). Nation: USA. Agency: NASA Greenbelt. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: COBE. USAF Sat Cat: 20322 . COSPAR: 1989-089A. Apogee: 886 km (550 mi). Perigee: 873 km (542 mi). Inclination: 98.9000 deg. Period: 102.60 min. Summary: Cosmic Background Explorer; measured background galactic infrared radiation. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..

1991 November 18 - . 15:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 66 km (41 mi).

1992 November 18 - . 02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P. LV Configuration: MT-135P-R835.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi).

1993 November 18 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 739. LV Family: Trident. Launch Vehicle: Trident D-5. LV Configuration: Trident D-5 DASO.
  • PGW test launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1993 November 18 - . 13:54 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 367-01.
  • Gorizont 29 - . Payload: Gorizont s/n 41L. Mass: 2,125 kg (4,684 lb). Nation: Russia. Agency: MOM. Class: Communications. Type: Civilian communications satellite. Spacecraft: Gorizont . USAF Sat Cat: 22907 . COSPAR: 1993-072A. Apogee: 35,835 km (22,266 mi). Perigee: 35,800 km (22,200 mi). Inclination: 5.0000 deg. Period: 1,437.70 min. Gorizont 29 (18 November 1993) and 30 (20 May 1994) were launched for Rimsat, Ltd., to provide communications services in the Pacific region under an agreement signed in 1992 between Rimsat and the Applied Mechanics NPO. Gorizont 29 was located at 130 degrees E in accordance with a lease arrangement with Rimsat Corporation (using slots allocated to Tonga by the International Telecommunications Union). Intended for use under commercial conditions. Positioned in geosynchronous orbit at 130 deg E in 1993-1997; 161 deg E in 1997-1998; 130 deg E in 1999. As of 5 September 2001 located at 130.39 deg E drifting at 0.011 deg W per day. As of 2007 Mar 8 located at 168.05E drifting at 0.374W degrees per day.

1997 November 18 - . 11:14 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Resurs F-1M - . Nation: Russia. Agency: RAKA. Manufacturer: Kozlov. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs F1M. Decay Date: 1997-12-13 . USAF Sat Cat: 25059 . COSPAR: 1997-072A. Apogee: 238 km (147 mi). Perigee: 211 km (131 mi). Inclination: 82.3000 deg. Period: 89.00 min. Summary: Landed in Kazakstan Dec 13..

1997 November 18 - . 19:35 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.167GS.
  • SERTS-97 (08) Solar extreme ultraviolet mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

1998 November 18 - . 15:40 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.178NM.
  • Microgravity mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

1998 November 18 - . 23:00 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima T. LV Family: TR-1. Launch Vehicle: TR-1A. LV Configuration: TR-1A TR-1A-7.
  • Microgravity mission - . Nation: Japan. Agency: NASDA. Apogee: 100 km (60 mi).

1999 November 18 - . 01:55 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 Mk II.
  • LMS Ionosphere / meteorology mission - . Nation: India. Agency: ISRO. Apogee: 135 km (83 mi).

2002 November 18 - . 02:32 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.197UG.
  • ISIS Ultraviolet astronomy mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

2004 November 18 - . 10:45 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. Launch Pad: LC1?. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-26 (83).
  • Shiyan Weixing 2 - . Payload: TANSUO 2. Mass: 300 kg (660 lb). Nation: China. Agency: SISE. Manufacturer: DFH. Class: Earth. Type: Earth resources satellite. Spacecraft: Shiyan Weixing. USAF Sat Cat: 28479 . COSPAR: 2004-046A. Apogee: 711 km (441 mi). Perigee: 694 km (431 mi). Inclination: 98.2000 deg. Period: 98.80 min. Summary: Remote Sensing Technology..

2005 November 18 - .
  • Soyuz TMA-7 moved on ISS. - . Nation: USA. Related Persons: McArthur; Tokarev. Program: ISS. Flight: ISS EO-12. Summary: The ISS EO-12 crew boarded their Soyuz TMA-7 and undocked from the Pirs module at 08:46 GMT, flew around the station, and then docked with the Zarya module at 09:05 GMT. This cleared the hatch on the Pirs module for a future planned spacewalk..

2007 November 18 - .
  • ISS On-Orbit Status 11/18/07 - . Nation: USA. Related Persons: Malenchenko; Tani; Whitson. Program: ISS. Flight: ISS EO-16. Sunday -- off-duty day for CDR Whitson, FE-1 Malenchenko and FE-2 Tani.

    Ahead: Week 5 of Increment 16.

    The crew completed the mandatory CHeCS (Crew Health Care Systems) emergency/contingency medical OBT (on-board training) drill, a one-hour U.S. exercise designed to refresh crewmembers' acuity in applying HMS (Health Maintenance System) equipment like ACLS (Advanced Cardio Life Support) in an emergency. (The drill gives the crew the opportunity to work as a team in resolving a simulated medical emergency onboard ISS and to refresh their memory of on-orbit stowage & deployment locations, equipment use, and procedures. Setting up (but not actually operating/manipulating) onboard equipment such as the RSP (Respiratory Support Pack), ALSP (Advanced Life Support Pack), intubation kit, HMS defibrillator, all stowed in the Lab CHeCS rack, and the CMRS (Crew Medical Restraint System), Peggy, Yuri and Dan stepped through the ACLS algorithm manual to resolve a simulated medical emergency onboard ISS. Objectives of the exercise include practicing communication and coordination necessary to perform medical emergency procedures, locating appropriate emergency medical components, and determining each crewmember's individual method of delivering CPR (cardio-pulmonary resuscitation) in zero-G.) Additional Details: ISS On-Orbit Status 11/18/07.


2008 November 18 - .
  • EVA STS-126-1 - . Crew: Stefanyshyn-Piper; Bowen. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.29 days. Nation: USA. Related Persons: Stefanyshyn-Piper; Bowen. Program: ISS. Flight: STS-126; ISS EO-18. Summary: The crew began the multi-EVA process of repair and lubrication of the errant Solar Alpha Rotary Joint. A 14-kg tool bag floated away and could not be recovered, but the work could be completed with spare tools..

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