Encyclopedia Astronautica
October 03


October 03 Chronology


1815 October 3 - .
  • Chassigny Meteorite Fall (Mars Meteorite) - . Nation: France.

1935 October 3 - .
1936 October 3 - . LV Family: Goddard. Launch Vehicle: Goddard L-A.
  • Flight of Goddard series L section A rocket - . Nation: USA. Related Persons: Goddard. Apogee: 0.0600 km (0.0373 mi). Summary: Rocket achieved 200 ft vertically in 5 sec, then combustion chamber burned through; weight oxygen 40 lb; weight gasoline 46 lb; weight nitrogen 4 lb; fell 20 ft from tower..

1942 October 3 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-004.
  • V-2 4004 - . Nation: Germany. Agency: Wehrmacht. Summary: Steep climb. Range 190 km .

1944 October 3 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-235. FAILURE: Failure.
1945 October 3 - .
  • US Navy studies satellite launcher. - . Nation: USA. Summary: A Navy Committee for Evaluating the Feasibility of Space Rocketry (CEFSR) was established by BuAer. In November 1945, CEFSR recommended high priority for satellite development and estimated cost between $5 and $8 million..

1947 October 3 - .
  • XS-1 Flight 47 - . Crew: Yeager. Payload: XS-1 # 1 flight 28. Nation: USA. Related Persons: Yeager. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF flight 6. Check of elevator and stabilizer effectiveness. Also buffet investigation..

1949 October 3 - .
1949 October 3 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1. LV Configuration: R-1 II-14.
  • Test mission - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1951 October 3 - .
  • Birth of Dr Kathryn Dwyer 'Kathy' Sullivan - . Nation: USA. Summary: American geologist mission specialist astronaut. Flew on STS-41-G, STS-31, STS-45. Geologist, first American woman to walk in space. As of 1999 Ms Sullivan was Director of the Center of Science and Industry in Columbus, Ohio..

1952 October 3 - . Launch Site: Wallops Island. LV Family: HVAR. Launch Vehicle: HVAR FFAR.
  • E39 Model test flight - . Nation: USA. Agency: NASA. Apogee: 1.00 km (0.60 mi).

1952 October 3 - . Launch Site: Wallops Island. LV Family: HVAR. Launch Vehicle: HVAR FFAR.
  • E39 Model test flight - . Nation: USA. Agency: NASA. Apogee: 2.00 km (1.20 mi).

1956 October 3 - .
  • X-1E Flight 13 - . Crew: Walker, Joseph. Payload: X-1E flight 13. Nation: USA. Related Persons: Walker, Joseph. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1E. Summary: NACA flight 12. Only 60-sec rocket operation; intermittent pump operation. Flight aborted, turbopump and engine replaced..

1957 October 3 - . Launch Site: Eniwetok. Launch Platform: Balloon. LV Family: Rockoon. Launch Vehicle: Farside.
  • Shot 2 Test/Ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 800 km (490 mi).

1957 October 3 - . 17:13 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Thor DM-18. LV Configuration: Thor DM-18 107. FAILURE: Failure. Failed Stage: 1.
  • Series I research and development launch - . Nation: USA. Agency: USAF. Apogee: 0 km ( mi).

1958 October 3 - . 03:32 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100 (A-1).
  • Aeronomy mission - . Nation: USSR. Agency: MVS. Apogee: 85 km (52 mi).

1959 October 3 - . 11:03 GMT - . Launch Site: Eglin. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun AA6.202C.
  • Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 122 km (75 mi).

1960 October 3 - . LV Family: UR-200. Launch Vehicle: UR-200.
  • Chelomei acquires Myasishchev and Khrunichev OKBs. - . Nation: USSR. Related Persons: Chelomei; Myasishchev. Spacecraft: Raketoplan. Central Committee of the Communist Party and Council of Soviet Ministers Decree 1057-434 'On transfer of OKB-23 as Branch No. I of OKB-52 and on course of work on IS anti-satellite system' was issued. Chelomei acquired the OKB-23 of Vladimir Mikhailovich Myasishchev, (which had formerly designed heavy bombers), as well as the M K Khrunichev heavy aviation factory. Both of these organisations had a very high level of technical and manufacturing expertise, and assisted Chelomei in quickly moving ahead on his new space projects.

1961 October 3 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • S- IVB stage to have a single J-2 engine - . Nation: USA. Program: Apollo. The MSFC-STG Space Vehicle Board at NASA Headquarters discussed the S- IVB stage, which would be modified by the Douglas Aircraft Company to replace the six LR-115 engines with a single J-2 engine. Funds of $500,000 were allocated for this study to be completed in March 1962. Additional Details: S- IVB stage to have a single J-2 engine.

1961 October 3 - . 18:40 GMT - . Launch Site: Silver Lake DZ. Launch Pad: 35.3 N x 116.1 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-23-39.
  • X-15A VO Stability test - . Nation: USA. Agency: NASA; USAF. Apogee: 23 km (14 mi). Summary: Flight made with lower ventral off. Maximum Speed - 4553 kph. Maximum Altitude - 23770 m..

1962 October 3 - .
  • Zagami Meteorite Fall (Mars Meteorite) - . Nation: Nigeria.

1962 October 3 - . 12:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC14. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 113D.
  • Mercury MA-8 - . Call Sign: Sigma 7. Crew: Schirra. Backup Crew: Cooper. Payload: Mercury SC16. Mass: 1,374 kg (3,029 lb). Nation: USA. Related Persons: Schirra; Cooper. Agency: NASA. Program: Mercury. Class: Manned. Type: Manned spacecraft. Flight: Mercury MA-8. Spacecraft: Mercury. Duration: 0.38 days. Decay Date: 1962-10-03 . USAF Sat Cat: 433 . COSPAR: 1962-B-Delta-1. Apogee: 285 km (177 mi). Perigee: 153 km (95 mi). Inclination: 32.5000 deg. Period: 88.80 min. The Sigma 7 spacecraft with Astronaut Walter M. Schirra, Jr., as pilot was launched into orbit by a Mercury-Atlas vehicle from Atlantic Missile Range. In the most successful American manned space flight to date, Schirra traveled nearly six orbits, returning to earth at a predetermined point in the Pacific Ocean 9 hours, 13 minutes after liftoff. Within 40 minutes after landing, he and his spacecraft were safely aboard the aircraft carrier U.S.S. Kearsarge. Schirra attempted and achieved a nearly perfect mission by sticking rigorously to mission plan.

1963 October 3 - . 03:30 GMT - . Launch Site: McMurdo Station. LV Family: Arcas. Launch Vehicle: Arcas.
  • McMurdo 28 Aeronomy mission - . Nation: USA. Apogee: 60 km (37 mi).

1964 October 3 - .
  • Voskhod integration problems - . Nation: USSR. Related Persons: Korolev. Program: Voskhod. Flight: Voskhod 1. Spacecraft: Voskhod. Work on completing the spacecraft is finally on schedule, but then it is found that there is a failure in the Signal device, which provides communications after the separation of the capsule from the equipment section after retrofire. Nevertheless it is decided to continue according to schedule and roll the booster and spacecraft out to the pad the next morning. Korolev has spent the day at Fedosiya, where the Voskhod landing system has finally completed a successful end-to-end test after being dropped from an aircraft at 10 km altitude.

1966 October 3 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. LV Family: Veronique. Launch Vehicle: Veronique 61M. LV Configuration: Veronique 61M VA77.
  • FU-145 ionosphere Magnetosphere / ionosphere / astronomy mission - . Nation: France. Agency: CNES. Apogee: 166 km (103 mi). Summary: FU145 Technology + Ionosphere / Stab mission..

1966 October 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 578.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 October 3 - . LV Family: Saturn I; Saturn V.
  • Budgetary cutbacks reduced AAP lunar activity to four missions and Saturn V Workshops to 17 Saturn IB and 7 Saturn V launches. - . Nation: USA. Spacecraft: Orbital Workshop; Skylab; AES Lunar Base; ALSS Lunar Base. NASA Hq issued a revised AAP schedule incorporating recent budgetary cutbacks. The schedule reflected the reduction of AAP lunar activity to four missions and of Saturn V Workshop activity to 17 Saturn IB and 7 Saturn V launches. There would be two Workshops launched on Saturn IBs, one Saturn V Workshop, and three ATMs. Launch of the first Workshop was scheduled for March 1970.

1967 October 3 - .
  • Mishin's errors means Kamanin will not see a Soviet man on the moon in his lifetime. - . Nation: USSR. Related Persons: Mishin. Program: Lunar L1; Lunar L3. Summary: The moon landing has already been delayed three to four years due to the mistakes of Mishin. Kamanin feels his mortality, the limited number of years remaining in his life, and is furious that Mishin is wasting time when life is so short for everyone..

1967 October 3 - . Launch Site: Johnston Island. LV Family: Sandhawk. Launch Vehicle: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia 281-8.
  • Aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 423 km (262 mi).

1967 October 3 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-103.
  • LASL Solar Solar mission - . Nation: USA. Agency: Sandia. Apogee: 309 km (192 mi).

1967 October 3 - . Launch Site: Baikonur. Launch Complex: Baikonur LC60/7. LV Family: R-16. Launch Vehicle: R-16U.
  • Combat training launch - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1967 October 3 - . 05:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-06 - . Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1. Decay Date: 1969-03-04 . USAF Sat Cat: 2973 . COSPAR: 1967-095A. Apogee: 39,709 km (24,673 mi). Perigee: 508 km (315 mi). Inclination: 64.7000 deg. Period: 714.90 min. Summary: Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network..

1967 October 3 - . 18:18 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.152GS.
  • Solar pointing Solar x-ray / ultraviolet mission - . Nation: USA. Agency: NASA. Apogee: 184 km (114 mi).

1967 October 3 - . 21:31 GMT - . Launch Site: Mud Lake DZ. Launch Pad: 37.9 N x 117.1 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 2-53-97. FAILURE: Heat flow from dummy ramjet nearly burns tail off..
  • X-15A-2 TPS/Ramjet/Mach 6.7 test - . Nation: USA. Agency: NASA; USAF. Apogee: 31 km (19 mi). Summary: Unofficial world speed record (full ablative coating, dummy ramjet, mechanical eyelid). Maximum Speed - 7273 kph. Maximum Altitude - 31120 m..

1968 October 3 - .
  • Apollo 7 flight readiness review - . Nation: USA. Program: Apollo. Flight: Apollo 7. Senior management from NASA Hq. and the three manned Centers conducted the Apollo 7 flight readiness review at KSC. Crew, space vehicle, and all supporting elements were ready for flight. Countdown-to-launch sequence had started on October 6, and flight preparations were on schedule for launch readiness at 11:00 a.m. EDT on October 11.

1968 October 3 - .
  • HL-10 Flight 11 - . Crew: Manke. Payload: HL-10 flight 11. Nation: USA. Related Persons: Manke. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: HL-10. Summary: Maximum Speed - 758 kph. Maximum Altitude - 13720 m. Flight Time - 243 sec..

1968 October 3 - .
  • Zond 5 arrives in Bombay - . Nation: USSR. Program: Lunar L1. Spacecraft: Soyuz 7K-L1. Summary: The vessel Vasiliy Golovnin docks at Bombay with the L1 capsule..

1968 October 3 - . 12:58 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 245 - . Payload: DS-P1-Yu s/n 16. Mass: 325 kg (716 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-Yu. Completed Operations Date: 1969-01-16 . Decay Date: 1969-01-15 . USAF Sat Cat: 3457 . COSPAR: 1968-083A. Apogee: 473 km (293 mi). Perigee: 284 km (176 mi). Inclination: 71.0000 deg. Period: 92.10 min. Summary: Development of systems for air defence and the control of outer space..

1968 October 3 - . 20:49 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout B. LV Configuration: Scout B S167C.
  • ESRO 1A - . Payload: Aurorae. Mass: 81 kg (178 lb). Nation: Europe. Agency: ESRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: ESRO. Decay Date: 1970-06-26 . USAF Sat Cat: 3459 . COSPAR: 1968-084A. Apogee: 1,538 km (955 mi). Perigee: 258 km (160 mi). Inclination: 93.8000 deg. Period: 103.00 min. Summary: Aurora, polar ionosphere investigations. .

1969 October 3 - .
  • Mishin arrives at Tyuratam. - . Nation: USSR. Related Persons: Mishin. Program: Soyuz. Flight: Soyuz 6; Soyuz 7; Soyuz 8. Summary: Kamanin notes he now always shows up only after the State Commission has met..

1969 October 3 - . 01:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1173.
  • FOT GT44B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 October 3 - . 02:24 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 04.279UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 158 km (98 mi).

1970 October 3 - .
  • DOS issues reviewed by VVS. - . Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Summary: Kamanin meets with the General Staff to discuss issues with the DOS trainer. The issue of forming crews for the DOS program consisting only of unflown cosmonauts is debated..

1970 October 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • OT GT46M operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 October 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-27 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 October 3 - . Launch Site: Kwajalein. Launch Complex: Kwajalein Meck. Launch Vehicle: Spartan.
  • Safeguard M1-27 Interceptor mission - . Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

1970 October 3 - . 04:20 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5V.
  • RAO K-2 Solar x-ray mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1970 October 3 - . 10:26 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 367 - . Mass: 3,800 kg (8,300 lb). Nation: USSR. Agency: PKO. Program: RORSAT. Class: Surveillance. Type: Military naval surveillance radar satellite. Spacecraft: US-A. Decay Date: 1970-10-31 . USAF Sat Cat: 4566 . COSPAR: 1970-079C. Apogee: 1,022 km (635 mi). Perigee: 915 km (568 mi). Inclination: 65.3000 deg. Period: 104.50 min. Summary: Ocean surveillance; probably used chemical batteries..

1971 October 3 - . 15:30 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1972 October 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • FOT GT109M Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1973 October 3 - . 02:27 GMT - . Launch Site: White Sands. LV Family: Astrobee. Launch Vehicle: Astrobee D. LV Configuration: Astrobee D CRL A30.311-2.
  • Infrared Radiometer Aeronomy mission - . Nation: USA. Agency: USAF CRL. Apogee: 100 km (60 mi).

1973 October 3 - . 06:00 GMT - . Launch Site: White Sands. LV Family: Astrobee. Launch Vehicle: Astrobee D. LV Configuration: Astrobee D CRL A30.311-3.
  • Infrared Radiometer Aeronomy mission - . Nation: USA. Agency: USAF CRL. Apogee: 102 km (63 mi).

1973 October 3 - . 06:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • FOT GT116M Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1973 October 3 - . 13:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 596 - . Payload: FEU-170 s/n 1L. Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 6.00 days. Decay Date: 1973-10-09 . USAF Sat Cat: 6856 . COSPAR: 1973-070A. Apogee: 287 km (178 mi). Perigee: 206 km (128 mi). Inclination: 65.4000 deg. Period: 89.40 min. Area survey photo reconnaissance satellite; returned film capsule. First test of small film return capsules planned for Yantar spacecraft. SpK capsule FEU-170 No. 1L experienced an electrical short circuit, which led to failure to separate the shell of the capsule after reentry, preventing parachute deployment. The capsule crashed into the ground.
  • Cosmos 596 Nauka - . Payload: FEU-170 s/n 1L. Nation: USSR. Agency: RVSN. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Nauka. Decay Date: 1973-10-09 . USAF Sat Cat: 6856 . COSPAR: 1973-070xx. Apogee: 273 km (169 mi). Perigee: 206 km (128 mi). Inclination: 65.4000 deg. Period: 89.30 min.

1974 October 3 - . Launch Site: Baikonur. Launch Complex: Baikonur LC162/36. LV Family: Tsiklon. Launch Vehicle: R-36 8K67. FAILURE: Failure.
  • OS state trials flight - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1974 October 3 - . 05:10 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.37GG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 250 km (150 mi).

1975 October 3 - . Launch Site: Marambio. LV Family: Canopus. Launch Vehicle: Castor (A).
1975 October 3 - . 03:15 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.47DH.
  • X-ray astronomy mission - . Nation: USA. Agency: NASA. Apogee: 212 km (131 mi).

1977 October 3 - . 14:47 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1978 October 3 - . 11:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1033 - . Payload: Zenit-4MKT no. 7. Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MKT. Duration: 13.00 days. Decay Date: 1978-10-16 . USAF Sat Cat: 11039 . COSPAR: 1978-089A. Apogee: 231 km (143 mi). Perigee: 212 km (131 mi). Inclination: 81.4000 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..

1978 October 3 - . 23:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Progress 4 - . Payload: Progress s/n 105. Mass: 7,014 kg (15,463 lb). Nation: USSR. Agency: MOM. Program: Salyut 6. Class: Manned. Type: Manned logistics spacecraft. Flight: Salyut 6 EO-2. Spacecraft: Progress. Duration: 22.72 days. Completed Operations Date: 1978-10-27 16:27:43 . Decay Date: 1978-10-27 16:27:43 . USAF Sat Cat: 11040 . COSPAR: 1978-090A. Apogee: 247 km (153 mi). Perigee: 185 km (114 mi). Inclination: 51.7000 deg. Period: 88.80 min. Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 6 Oct 1978 01:00:15 GMT. Undocked on 24 Oct 1978 13:01:52 GMT. Destroyed in reentry on 26 Oct 1978 16:28:13 GMT. Total free-flight time 4.22 days. Total docked time 18.50 days.

1979 October 3 - . 17:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 302-02.
  • Ekran 4 - . Payload: Ekran s/n 17L. Mass: 1,970 kg (4,340 lb). Nation: USSR. Agency: MOM. Class: Communications. Type: Military communications satellite. Spacecraft: Ekran . Completed Operations Date: 1981-03-01 . USAF Sat Cat: 11561 . COSPAR: 1979-087A. Apogee: 35,827 km (22,261 mi). Perigee: 35,725 km (22,198 mi). Inclination: 14.5000 deg. Period: 1,435.60 min. Transmission of color and black-and-white USSR central television programmes to a network of receivers for collective use. Positioned in geosynchronous orbit at 99 deg E in 1979-1981 As of 4 September 2001 located at 52.52 deg E drifting at 0.007 deg W per day. As of 2007 Mar 4 located at 96.71E drifting at 0.048W degrees per day.

1979 October 3 - . 18:42 GMT - . Launch Site: El Arenosillo. LV Family: Petrel. Launch Vehicle: Petrel 2. LV Configuration: Petrel 2 P218E.
  • Plasma injection Ionosphere mission - . Nation: UK. Agency: SRC. Apogee: 145 km (90 mi).

1980 October 3 - . 12:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1213 - . 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: 1980-10-17 . USAF Sat Cat: 11997 . COSPAR: 1980-080A. Apogee: 313 km (194 mi). Perigee: 192 km (119 mi). Inclination: 72.9000 deg. Period: 89.60 min. Summary: Photo surveillance; returned film capsule; maneuverable..

1983 October 3 - . 18:34 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 728. LV Family: Trident. Launch Vehicle: Trident C-4.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1984 October 3 - . 14:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Pershing. Launch Vehicle: Pershing 2.
  • Operational test - . Nation: USA. Agency: USA. Apogee: 250 km (150 mi).

1985 October 3 - . 05:48 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92M.
  • Cosmos 1689 - . Payload: Resurs-O1 no. 1. Mass: 1,500 kg (3,300 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs-O1. Decay Date: 2001-01-14 . USAF Sat Cat: 16110 . COSPAR: 1985-090A. Apogee: 545 km (338 mi). Perigee: 496 km (308 mi). Inclination: 97.6000 deg. Period: 95.10 min. First flight of Resurs-O1. Acquisition of operational information on the natural resources of the earth in the interests of various branches of the national economy of the USSR; continued trials of new types of informational and measurement apparatus and methods of remote sensing of the earth's surface and atmosphere. Operated for one year, two months. Re-entered January 14, 2001.

1985 October 3 - . 07:33 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
  • Molniya 3-26 - . Payload: Molniya-3 s/n 38. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-3. Decay Date: 2001-02-22 . USAF Sat Cat: 16112 . COSPAR: 1985-091A. Apogee: 38,722 km (24,060 mi). Perigee: 1,660 km (1,030 mi). Inclination: 64.6000 deg. Period: 718.40 min. Summary: Operation of the long-range telephone and telegraph radio communications system in the USSR; transmission of USSR Central Television programmes to stations in the Orbita network and within the framework of international cooperation. .

1985 October 3 - . 15:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-28/51-J.
  • STS-51-J - . Call Sign: Atlantis. Crew: Bobko; Grabe; Hilmers; Pailes; Stewart. Payload: Atlantis F01 / DSCS-3 2 / DSCS-3 3 [IUS]. Nation: USA. Related Persons: Bobko; Grabe; Hilmers; Pailes; Stewart. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-51-J. Spacecraft: Atlantis. Duration: 4.07 days. Decay Date: 1985-10-07 . USAF Sat Cat: 16115 . COSPAR: 1985-092A. Apogee: 486 km (301 mi). Perigee: 476 km (295 mi). Inclination: 28.5000 deg. Period: 94.20 min. Manned five crew. Atlantis (first flight); deployed USA 11, USA 12. Reusable space transportation system.

    Orbits of Earth: 63. Landed at: Runway 23 dry lake bed at Edwards Air Force Base, . Touchdown miss distance: 754.00 m. Landing Rollout: 2,455.00 m. Payloads: Classified DoD Mission - Record altitude (as of 5/93).

  • USA 11 - . Payload: DSCS III F-2. Nation: USA. Agency: USAF. Program: DSCS. Class: Communications. Type: Military communications satellite. Spacecraft: DSCS III. USAF Sat Cat: 16116 . COSPAR: 1985-092B. Apogee: 35,963 km (22,346 mi). Perigee: 35,434 km (22,017 mi). Inclination: 0.3000 deg. Period: 1,436.00 min. Summary: Released from STS 51J 10/4/85. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit; at 12 deg W in 1986; 42 deg W in 1995..
  • USA 12 - . Payload: DSCS III F-3. Nation: USA. Agency: USAF. Program: DSCS. Class: Communications. Type: Military communications satellite. Spacecraft: DSCS III. USAF Sat Cat: 16117 . COSPAR: 1985-092C. Apogee: 35,963 km (22,346 mi). Perigee: 35,633 km (22,141 mi). Inclination: 0.3000 deg. Period: 1,436.00 min. Released from STS 51J 4 October 1985; boosted into orbit with DSCS 3 F3 on single IUS booster. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit; at 180 deg E in 1994.

1986 October 3 - . 13:05 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL. FAILURE: Fourth stage failure.. Failed Stage: 3.
  • Cosmos 1783 - . Payload: Oko #49. Mass: 1,800 kg (3,900 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. USAF Sat Cat: 16993 . COSPAR: 1986-075A. Apogee: 18,679 km (11,606 mi). Perigee: 1,970 km (1,220 mi). Inclination: 64.6000 deg. Period: 358.00 min. Summary: Unusable orbit. Was intended to cover Oko constellation plane 1 - 272 degree longitude of ascending node..

1988 October 3 - . 22:23 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Cosmos 1974 - . Payload: Oko #58. Mass: 1,250 kg (2,750 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. USAF Sat Cat: 19554 . COSPAR: 1988-092A. Apogee: 33,413 km (20,761 mi). Perigee: 6,942 km (4,313 mi). Inclination: 68.0000 deg. Period: 717.80 min. Summary: Covered Oko constellation plane 7 - 157 degree longitude of ascending node..

1988 October 3 - .
1989 October 3 - . 14:59 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2047 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 49.00 days. Decay Date: 1989-11-21 . USAF Sat Cat: 20279 . COSPAR: 1989-082A. Apogee: 330 km (200 mi). Perigee: 165 km (102 mi). Inclination: 67.1000 deg. Period: 89.50 min. Summary: High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1990 October 3 - .
  • East and West Germany reunited. - . Nation: Germany.

1991 October 3 - .
  • Death of Joseph Kaplan - . Nation: USA. Related Persons: Kaplan. Summary: Hungarian-American geophysicist, heavily involved in efforts in the 1950s to launch the first satellite, served as the chair of the US National Committee for the International Geophysical Year, 1953-1963..

1991 October 3 - . 22:27 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-194.
  • Turbo-Metal Aeronomy mission - . Nation: Germany. Agency: DLR. Apogee: 140 km (80 mi).

1994 October 3 - . 22:42 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Soyuz TM-20 - . Call Sign: Vityaz (Knight ). Crew: Kondakova; Merbold; Viktorenko. Backup Crew: Budarin; Reiter; Solovyov. Payload: Soyuz TM 11F732 s/n 69. Mass: 7,150 kg (15,760 lb). Nation: Russia. Related Persons: Kondakova; Merbold; Viktorenko; Budarin; Reiter; Solovyov. Agency: MOM. Program: Mir. Class: Manned. Type: Manned spacecraft. Flight: Mir EO-17; Mir Euromir 94; Mir EO-16; Mir LD-4. Spacecraft: Soyuz TM. Duration: 169.22 days. Decay Date: 1995-03-02 . USAF Sat Cat: 23288 . COSPAR: 1994-063A. Apogee: 395 km (245 mi). Perigee: 392 km (243 mi). Inclination: 51.6000 deg. Period: 92.43 min. Mir Expedition EO-17. Docked at the Mir forward port at 00:28 on 1994 October 6. The Mir crew of Viktorenko, Kondakova and Polyakov boarded Soyuz TM-20 on January 11, and undocked from Mir's front port at 09:00 GMT. The spacecraft withdrew to about two hundred metres from Mir and then redocked in a test of the automatic Kurs system, which had failed in Progress M-24's attempted docking. Redocking came at 09:25 GMT.

1995 October 3 - .
  • Astronaut Charles Lacy Veach dies at age of 51 -- Natural causes - Cancer. - . Nation: USA. Related Persons: Veach. Summary: American engineer mission specialist astronaut. Flew on STS-39, STS-52..

1996 October 3 - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Shtil.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1996 October 3 - . Launch Site: Plesetsk. LV Family: Topol. Launch Vehicle: Topol.
  • Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1997 October 3 - . 07:07 GMT - . Launch Site: Plesetsk. LV Family: Topol. Launch Vehicle: Topol.
  • Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1998 October 3 - . 10:04 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576E. LV Family: Pegasus. Launch Vehicle: ARPA Taurus. LV Configuration: ARPA Taurus T3 1110.
  • STEX - . Payload: STEX. Nation: USA. Agency: NRO. Manufacturer: NRL. Class: Technology. Type: Ion engine technology satellite. Spacecraft: STEX. USAF Sat Cat: 25489 . COSPAR: 1998-055A. Apogee: 759 km (472 mi). Perigee: 744 km (462 mi). Inclination: 84.9859 deg. Period: 99.77 min. Tested TAL-D55 plasma engine and was to be part of the NRO's ATex tether experiment. The ATeX lower end mass was meant to remain attached to the STEX parent spacecraft, but with only 21 m of tether deployed, it appeared the tether was so far off vertical that automatic safety systems jettisoned the base to protect the remainder of the STEX satellite. Thus, the upper and lower ATeX end masses were in orbit as one object connected by a 21 m tether, and designated USA 141 (1998-055C). The main STEX satellite was in orbit as a separate object, 1998-055A.
  • USA 141 - . Payload: ATEX. Nation: USA. Agency: NRO; NRL. Class: Technology. Type: Tether technology satellite. Spacecraft: TiPS. USAF Sat Cat: 25615 . COSPAR: 1998-055C. Apogee: 766 km (476 mi). Perigee: 750 km (466 mi). Inclination: 84.9910 deg. Period: 99.90 min. NRO's ATeX (Advanced Tether eXperiment) reportedly failed on January 16. The ATeX lower end mass was meant to remain attached to the STEX parent spacecraft, but with only 21 m of tether deployed, it appeared the tether was so far off vertical that automatic safety systems jettisoned the base to protect the remainder of the STEX satellite. Thus, the upper and lower ATeX end masses were in orbit as one object connected by a 21 m tether, and designated USA 141 (1998-055C). The main STEX satellite was in orbit as a separate object, 1998-055A.

1999 October 3 - . 02:01 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 MSLS IFT-3.
  • MSLS IFT-3 Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi). The only decoy used in IFT-3 was the large balloon from IFT-1A and IFT-2. It had an IR signature six times higher than that of the mock warhead. Because the decoy was so much brighter than the mock warhead, the EKV saw it first. Once the EKV realized that the balloon’s IR signature did not match the target data loaded prior to the test, the interceptor shifted to the nearby target.

1999 October 3 - . 02:22 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein Meck. LV Family: Minuteman. Launch Vehicle: Payload Launch Vehicle. LV Configuration: Minuteman 2 PLV PLV.
  • IFT-3 EKV ABM test - . Nation: USA. Agency: USA SSDC. Apogee: 230 km (140 mi). EKV anti-ballistic missile interceptor launched from Kwajalein Atoll by a two-stage PLV. Intercept of the MSLS launched by Minuteman 2 from Vandenberg was successful. Element test of the EKV, not an end-to-end system test, which relied on a surrogate booster vehicle and range assets to define the deployment basket and deliver the EKV to that location. Once deployed, the EKV operated autonomously to intercept the mock RV. Due to a malfunctioning Inertial Measurement Unit (IMU), which normally was used to position the EKV for the intercept, a backup method of locating the target had to be exercised. The EKV called upon its step-stare capabilities (which were used only during off-nominal circumstances) to extend its field of view since the target was not where it was anticipated. After executing that procedure, the EKV acquired its target.

2001 October 3 - . 09:00 GMT - . Launch Site: Plesetsk. LV Family: Topol. Launch Vehicle: Topol.
  • Operational test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

2003 October 3 - . 14:30 GMT - . Launch Site: Wallops Island. LV Family: Terrier. Launch Vehicle: Terrier Orion Improved. LV Configuration: Terrier Improved Orion NASA 41.035UE.
  • SPIRIT 2 Aeronomy / Chemical release mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 130 km (80 mi).

2005 October 3 - .
2009 October 3 - .
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