Encyclopedia Astronautica
October 21


October 21 Chronology


1897 October 21 - .
  • Yerkes Observatory founded. - . Nation: USA.

1942 October 21 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-005.
  • V-2 4005 - . Nation: Germany. Agency: Wehrmacht. Summary: Steam generator fault. Range 147 km..

1943 October 21 - . Launch Site: Peenemuende. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-067.
1944 October 21 - . Launch Site: V-2 Battery 444. LV Family: V-2. Launch Vehicle: V-2.
  • V-2 Batteries 1./444, 2./444 and 3./444 move from Rijs to The Hague. - . Nation: Germany. Agency: Wehrmacht.

1947 October 21 - .
  • XS-1 Flight 51 - . Crew: Hoover. Payload: XS-1 # 2 flight 20. Nation: USA. Related Persons: Hoover. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: NACA glide-familiarization flight for NACA pilot. Stall check. Nosewheel collapsed on landing..

1948 October 21 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1. LV Configuration: R-1 I-6.
  • Test mission - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1950 October 21 - .
  • Birth of Dr Ronald Erwin McNair - . Nation: USA. Summary: African-American physicist mission specialist astronaut. Flew on STS-41-B, STS-51-L. Died in Challenger accident..

1950 October 21 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-2. Launch Vehicle: R-2. LV Configuration: R-2 1.
  • First series test launch - . Nation: USSR. Agency: Korolev. Apogee: 150 km (90 mi). Summary: First launch in first test series of protoype missiles..

1952 October 21 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 124R.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1953 October 21 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Hermes. Launch Vehicle: Hermes A-3A. LV Configuration: Hermes A-3A 5.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 30 km (18 mi).

1958 October 21 - . LV Family: Little Joe. Launch Vehicle: Little Joe.
  • Bidders' briefing for the Mercury Little Joe launch vehicle. - . Nation: USA. Program: Mercury. A bidders' briefing for the Little Joe launch vehicle was held. As earlier mentioned, this launch vehicle was to be used in the development phase of the manned satellite project. The Little Joe launch vehicle was 48 feet in height, weighed (at maximum) 41,330 pounds, was 6.66 feet in diameter, consisted of four Pollux and four Recruit clustered, solid-fuel rockets, could develop a thrust of 250,000 pounds, and could lift a maximum payload of 3,942 pounds.

1959 October 21 - . LV Family: Saturn I. Launch Vehicle: Saturn I.
  • Transfer to NASA of the Army Ballistic Missile Agency's Development Operations Division - . Nation: USA. Related Persons: von Braun; Eisenhower. Program: Apollo. After a meeting with officials concerned with the missile and space program, President Dwight D. Eisenhower announced that he intended to transfer to NASA control the Army Ballistic Missile Agency's Development Operations Division personnel and facilities. The transfer, subject to congressional approval, would include the Saturn development program.

1959 October 21 - . 22:57 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 220.
  • IWST - . Nation: USA. Agency: RAF. Apogee: 520 km (320 mi).

1960 October 21 - .
  • Design constraints for in-house study of the Apollo spacecraft - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Summary: A staff meeting of STG's Flight Systems Division was held to fix additional design constraints for the in- house design study of the Apollo spacecraft.

    Fundamental decisions were made as a result of this and a previous meeting on September 20.. Additional Details: Design constraints for in-house study of the Apollo spacecraft.


1960 October 21 - .
  • Evaluation completed on proposals for an advanced manned spacecraft - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Source Selection. The Technical Assessment Panels presented to the Evaluation Board their findings on the contractors' proposals for feasibility studies of an advanced manned spacecraft. On October 24, the Evaluation Board findings and recommendations were presented to the STG Director.

1961 October 21 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5A.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1961 October 21 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5A.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1961 October 21 - . 13:53 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 105D.
  • Midas 4 - . Payload: Midas / Agena TV 1202. Mass: 1,800 kg (3,900 lb). Nation: USA. Agency: USAF. Class: Military. Type: Early warning satellite. Spacecraft: Midas. USAF Sat Cat: 192 . COSPAR: 1961-A-Delta-1. Apogee: 3,763 km (2,338 mi). Perigee: 3,482 km (2,163 mi). Inclination: 95.9000 deg. Period: 165.90 min. Summary: Missile Defense Alarm System. Deployed subsatellites..
  • Westford - . Payload: Westford. Nation: USA. Agency: USAF. Spacecraft: WestFord Needles. USAF Sat Cat: 194 . COSPAR: 1961-A-Delta-3.

1962 October 21 - . Launch Site: Barking Sands. LV Family: Honest John. Launch Vehicle: HJ Nike.
  • Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).

1963 October 21 - .
  • The second prototype space suit was received by MSC's Crew Systems Division - . Nation: USA. Related Persons: Young. Program: Apollo. Spacecraft: Apollo CSM; A7L; CSM Hatch. The second prototype space suit was received by MSC's Crew Systems Division. Preliminary tests showed little improvement in mobility over the first suit. On October 24-25, a space suit mobility demonstration was held at North American. The results showed that the suit had less shoulder mobility than the earlier version, but more lower limb mobility. Astronaut John W. Young, wearing the pressurized suit and a mockup portable life support system (PLSS), attempted an egress through the CM hatch but encountered considerable difficulty. At the same time, tests of the suit-couch- restraint system interfaces and control display layout were begun at the Navy's Aviation Medical Acceleration Laboratory centrifuge in Johnsville, Pa. Major problems were restriction of downward vision by the helmet, extension of the suit elbow arm beyond the couch, and awkward reach patterns to the lower part of the control panel. On October 30-November 1, lunar task studies with the suit were carried out at Wright-Patterson Air Force Base in a KC-135 aircraft at simulated lunar gravity. Mobility tests were made with the suit pressurized and a PLSS attached.

1964 October 21 - . 19:44 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA2. Launch Pad: LA2A. LV Family: Astrobee. Launch Vehicle: Astrobee 1500. LV Configuration: Astrobee 1500 NASA 16.02GT.
  • Test mission - . Nation: USA. Agency: NASA. Apogee: 1,950 km (1,210 mi).

1964 October 21 - . 21:12 GMT - . Launch Site: Carnarvon. Launch Complex: Carnarvon CARN. Launch Vehicle: HAD. LV Configuration: HAD 148.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi).

1965 October 21 - .
  • Bubble-type helmet for the Apollo extravehicular mobility unit - . Nation: USA. Program: Apollo. Spacecraft: A7L. MSC announced that the bubble-type helmet, designed by Crew Systems Division (CSD) engineers Robert L. Jones and James O'Kane, had been adopted for use in the Apollo extravehicular mobility unit. The new helmet was smaller and lighter than earlier types; extensive studies by CSD had demonstrated its superior comfort, visibility, and don/doff characteristics.

1965 October 21 - .
  • Planning schedule for follow-up procurement of Apollo spacecraft for the AAP. - . Nation: USA. Related Persons: Low, George. Spacecraft: Apollo X. MSC Deputy Director George M. Low advised NASA Hq of Houston's planning schedule for follow-up procurement of Apollo spacecraft for the AAP. Based upon the most recent delivery schedules for the last several command and service modules and lunar excursion modules for Apollo, contract award for those vehicles was scheduled for July and August 1966. In accordance with a 14 July directive from Headquarters, MSC was preparing a procurement plan for the extended CSM and the LEM derivatives covering both the final definition and development and operational phases of AAP. Approval of this plan by Headquarters, Low stated, was anticipated for mid-December, while award of contracts for the program definition phase was set for late January 1966. The contract award date for actual development of the extended CSM was slated for October 1966, while that for the LEM derivatives was postponed until mid- 1967 (in line with revised funding directives from Washington).

1965 October 21 - . LV Family: Saturn I. Launch Vehicle: Saturn IB.
  • Launch schedule for Apollo-Saturn IB flights revised - . Nation: USA. Related Persons: Phillips, Samuel. Program: Apollo. Spacecraft: Apollo CSM; CSM Block I. Samuel C. Phillips, Apollo Program Director, notified the Center directors and Apollo program managers in Houston, Huntsville, and Cape Kennedy that OMSF's launch schedule for Apollo-Saturn IB flights had been revised, based on delivery of CSMs 009 and 011:

    • AS-201 - January 1966
    • AS-202 - June 1966
    Schedules for AS-203 through 205 (July and October 1966, and January 1967) were unchanged.

1965 October 21 - . 16:00 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.164UA.
  • JHU Ikeya-Seki Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 191 km (118 mi).

1966 October 21 - .
1966 October 21 - . 20:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 914.
  • Follow-on operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 October 21 - .
  • Lunar crew controversy rages. - . Nation: USSR. Related Persons: Mishin; Anokhin; Feoktistov; Tyulin; Kerimov. Program: Lunar L3; Lunar L1. Spacecraft: Soyuz 7K-LOK. First Mishin was pushing the 60-year-old Anokhin for spaceflight, now the invalid Feoktistov. Feoktistiov suffers from gastrointestinal ulcers. Tyulin and Kerimov are of one voice in the matter - this is not even a question that can be raised - sick is sick, period. The L1 and L3 crews will have to endure eight to ten days of orbital flight. They can only be between 170 and 175 cm tall, and can have a maximum weight of 70 kg. Mishin insists that he doesn't even need military pilots for the L1 and L3, and therefore doesn't need to decide crew compositions until the middle of 1968, and then only 'his' engineer cosmonauts from TsKBEM should be considered. The Marshal interrupts Mishin, angrily reminding him that the space program is a national enterprise, not something being accomplished by 'your' spacecraft or 'your' cosmonauts. A three hour-long bitter debate ensues, with no resolution on crew selections. The final conclusions are only that the crews will consist of one pilot, and one engineer, and that Feoktistov will never be allowed to go into space.

1967 October 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF24. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2445.
  • ST Olympic Trials 4 operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1968 October 21 - .
1968 October 21 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 608. LV Family: Polaris. Launch Vehicle: Polaris A2E. LV Configuration: Polaris A2E A2E.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 October 21 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 608. LV Family: Polaris. Launch Vehicle: Polaris A2E. LV Configuration: Polaris A2E A2E.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 October 21 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 608. LV Family: Polaris. Launch Vehicle: Polaris A2E. LV Configuration: Polaris A2E A2E.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 October 21 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 608. LV Family: Polaris. Launch Vehicle: Polaris A2E. LV Configuration: Polaris A2E A2E.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 October 21 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 608. LV Family: Polaris. Launch Vehicle: Polaris A2E. LV Configuration: Polaris A2E A2E.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 October 21 - .
1969 October 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1134.
  • FOT GT45B Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 October 21 - . 12:32 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: 164 km (101 mi).

1969 October 21 - . 12:49 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. Launch Pad: LC132/pad?. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 304 - . Mass: 795 kg (1,752 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Tsiklon. USAF Sat Cat: 4138 . COSPAR: 1969-091A. Apogee: 748 km (464 mi). Perigee: 731 km (454 mi). Inclination: 74.0000 deg. Period: 99.60 min. Summary: Military navigation satellite..

1970 October 21 - . 09:39 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 106.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi).

1970 October 21 - . 13:25 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Ionosphere mission - . Nation: USSR. Apogee: 176 km (109 mi).

1970 October 21 - . 14:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Plasma mission - . Nation: USSR. Apogee: 150 km (90 mi).

1970 October 21 - . 15:03 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Ionosphere/Plasma mission - . Nation: USSR. Apogee: 168 km (104 mi).

1971 October 21 - . 11:32 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Delta N6. LV Configuration: Thor Delta N6 572/D86. FAILURE: Failure.. Failed Stage: 2.
  • ITOS B - . Payload: ITOS B. Mass: 308 kg (679 lb). Nation: USA. Agency: NASA Greenbelt. Program: Tiros. Class: Earth. Type: Weather satellite. Spacecraft: ITOS. Decay Date: 1972-07-21 . USAF Sat Cat: 5565 . COSPAR: 1971-091A. Apogee: 1,483 km (921 mi). Perigee: 293 km (182 mi). Inclination: 102.5000 deg. Period: 102.70 min. Summary: Unusable orbit..

1972 October 21 - . 12:34 GMT - . Launch Site: Barking Sands. Launch Complex: Barking Sands LC12. LV Family: Tomahawk Sandia. Launch Vehicle: Terrier Tomahawk. LV Configuration: Terrier Tomahawk Sandia 152-197.
  • LRL ACS-7B X-ray astronomy mission - . Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi).

1972 October 21 - . 13:16 GMT - . Launch Site: Poker Flat. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.151UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1972 October 21 - . 20:00 GMT - . Launch Site: Andoya. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P126A.
  • Particles / substorm Aurora mission - . Nation: UK. Agency: SRC. Apogee: 117 km (72 mi).

1973 October 21 - . 00:03 GMT - . Launch Site: Eglin. LV Family: Tomahawk Sandia. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.207-3. FAILURE: Failure.
  • Release Aeronomy mission - . Nation: USA. Agency: USAF CRL. Apogee: 18 km (11 mi).

1974 October 21 - . 20:00 GMT - . Launch Site: Poker Flat. Launch Vehicle: Rocketsonde.
  • Met Para, Datasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1975 October 21 - .
  • X-24 Flight 60 - . Crew: Scobee. Payload: X-24B flight 32. Nation: USA. Related Persons: Scobee. Class: Manned. Type: Manned spaceplane. Spacecraft: X-24B. Summary: Maximum Speed - 743 kph. Maximum Altitude - 13720 m. Flight Time - 255 sec..

1975 October 21 - . 11:42 GMT - . Launch Site: El Arenosillo. LV Family: INTA. Launch Vehicle: INTA-300. LV Configuration: INTA-300 F-75001.
  • Aeronomy / test - . Nation: Germany. Agency: INTA. Apogee: 240 km (140 mi). Summary: Failed to reach expected altitude..

1976 October 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC170. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100. FAILURE: Failure.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1976 October 21 - . 16:53 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 861 - . 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: 1977-02-04 . USAF Sat Cat: 9631 . COSPAR: 1976-104C. Apogee: 987 km (613 mi). Perigee: 928 km (576 mi). Inclination: 64.9000 deg. Period: 104.20 min. Summary: Ocean surveillance; nuclear powered..

1977 October 21 - . 08:49 GMT - . Launch Site: Kiruna. LV Family: Black Brant. Launch Vehicle: Black Brant 8C. LV Configuration: Black Brant 8C SSC S19B.
  • S19 Guidance test - . Nation: Sweden. Agency: SSC. Apogee: 374 km (232 mi).

1977 October 21 - . 10:05 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53716-325.
  • Cosmos 959 - . Payload: DS-P1-M. Mass: 650 kg (1,430 lb). Nation: USSR. Agency: MO. Class: Military. Type: Anti-satellite system target. Spacecraft: DS-P1-M. Decay Date: 1977-11-30 . USAF Sat Cat: 10419 . COSPAR: 1977-101A. Apogee: 850 km (520 mi). Perigee: 146 km (90 mi). Inclination: 65.8000 deg. Period: 94.60 min. Summary: ASAT target for Cosmos 961 interceptor..

1979 October 21 - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.08IU.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1979 October 21 - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.09IU.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1979 October 21 - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.10IU.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1981 October 21 - . 19:12 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 89 km (55 mi).

1982 October 21 - . 14:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47193-471.
  • Cosmos 1418 - . Mass: 550 kg (1,210 lb). Nation: USSR. Agency: MO. Class: Military. Type: Radar calibration target. Spacecraft: Taifun-1Yu. Decay Date: 1983-09-30 . USAF Sat Cat: 13627 . COSPAR: 1982-104A. Apogee: 414 km (257 mi). Perigee: 370 km (220 mi). Inclination: 50.7000 deg. Period: 92.40 min. Summary: Radar calibration mission..

1983 October 21 - . 12:10 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1505 - . 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: 1983-11-04 . USAF Sat Cat: 14425 . COSPAR: 1983-107A. Apogee: 337 km (209 mi). Perigee: 193 km (119 mi). Inclination: 72.9000 deg. Period: 89.80 min. Summary: Photo surveillance; returned film capsule..

1985 October 21 - . 05:04 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-7 (12).
  • FSW-0 No. 7 - . Payload: FSW-0 No. 07. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1985-11-07 . USAF Sat Cat: 16177 . COSPAR: 1985-096A. Apogee: 393 km (244 mi). Perigee: 171 km (106 mi). Inclination: 63.0000 deg. Period: 90.20 min. Summary: Fanhui Shi Weixing photo surveillance satellite; film capsule recovered 26 October..

1986 October 21 - . 22:07 GMT - . Launch Site: Barking Sands. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 68 km (42 mi).

1987 October 21 - . 21:28 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A Sphere.
  • MAC / EPSILON E-F2 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 113 km (70 mi).

1987 October 21 - . 21:33 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-149.
  • MAC / E-T3 Total 9 Aeronomy mission - . Nation: Norway. Agency: DLR. Apogee: 140 km (80 mi).

1987 October 21 - . 21:33 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-150.
  • MAC / E Aeronomy mission - . Nation: Germany. Agency: DLR. Apogee: 140 km (80 mi).

1987 October 21 - . 21:33 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.66UE.
  • MAC / Epsilon EXERT Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1987 October 21 - . 21:34 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.64GE.
  • Aeronomy mission - . Nation: Germany. Agency: NASA. Apogee: 140 km (80 mi).

1987 October 21 - . 21:46 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A Chaff.
  • MAC / EPSILON E-C6 / SL Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 101 km (62 mi).

1987 October 21 - . 23:21 GMT - . Launch Site: Andoya. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki Chaff.
  • MAC / EPSILON E-C8 / SL Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 102 km (63 mi).

1988 October 21 - . 14:35 GMT - . Launch Site: Zingst. Launch Vehicle: MMR-06. FAILURE: Failure..
  • MMR06-M Zingst launch 1 - . Nation: USSR. Agency: GMS. Apogee: 1.00 km (0.60 mi). Summary: Test launch. Earth impacted at 8 seconds. AES - R defective.

1989 October 21 - . 09:31 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 6925. LV Configuration: Delta 6925 D188.
  • USA 47 - . Payload: GPS 2-4 / GPS SVN 19. Mass: 1,665 kg (3,670 lb). Nation: USA. Agency: USAF. Manufacturer: Seal Beach. Program: Navstar. Class: Navigation. Type: Navigation satellite. Spacecraft: GPS Block 2 and 2A. USAF Sat Cat: 20302 . COSPAR: 1989-085A. Apogee: 21,236 km (13,195 mi). Perigee: 21,190 km (13,160 mi). Inclination: 53.3000 deg. Period: 760.20 min. Summary: Global Positioning System. Placed in Plane A Slot 5..

1992 October 21 - . 10:21 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Cosmos 2217 - . Payload: Oko #70. Mass: 1,900 kg (4,100 lb). Nation: Russia. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. Decay Date: 2010-11-07 . USAF Sat Cat: 22189 . COSPAR: 1992-069A. Apogee: 36,700 km (22,800 mi). Perigee: 3,642 km (2,263 mi). Inclination: 67.1000 deg. Period: 717.50 min. Summary: Covered Oko constellation plane 8 - 201 degree longitude of ascending node..

1993 October 21 - . 01:46 GMT - . Launch Site: El Arenosillo. LV Family: INTA. Launch Vehicle: INTA-300B. LV Configuration: INTA-300B IAA.
  • FEIROX / FEIROH Aeronomy mission - . Nation: Spain. Agency: INTA. Apogee: 154 km (95 mi).

1994 October 21 - .
  • Death of Jerome B Wiesner at Watertown, Middlesex, MA. - . Nation: USA. Related Persons: Wiesner. Summary: American scientist. Physicist, gadfly, science advisor to Presidents Eisenhower and Kennedy; opposed human spaceflight, the Apollo program, and the lunar orbit rendezvous method of lunar landing..

1996 October 21 - .
  • Death of Emerson W Conlon - . Nation: USA. Related Persons: Conlon. Summary: American engineer. Directed development of the D-558 transonic research aircraft for the Navy. Later Chair of the Aeronautical Engineerng Department at Michigan, holding several USAF and NASA management positions on leaves of absence..

1996 October 21 - . 03:00 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 36.115UG.
  • JHU FPT 1 (Jupiter) Ultraviolet astronomy mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

1997 October 21 - . 15:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 83 km (51 mi).

1998 October 21 - . 16:37 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5G. LV Configuration: Ariane 5G V112 (503).
  • Maqsat 3 - . Nation: France. Agency: ESA. Manufacturer: Kayser-Threde. Class: Technology. Type: Navigation technology satellite. Spacecraft: MAQSAT. USAF Sat Cat: 25503 . COSPAR: 1998-059A. Apogee: 35,491 km (22,053 mi). Perigee: 1,017 km (631 mi). Inclination: 7.5000 deg. Period: 641.20 min. Maqsat 3 was an instrumentation package used to monitor performance of the Ariane 5 booster. At T+12:43 the Speltra adapter cover separated revealing Maqsat-3. At T+15:14 the EPS stage Aestus engine ignited and burned until T+31:00. At this point on a normal mission the satellite would separate from the EPS, but to avoid creating space debris Maqsat remained attached to the EPS. The EPS/Maqsat-3 was placed in a 1027 km x 35863 km x 7.0 degree geostationary transfer orbit.
  • ARD - . Payload: Atmospheric Reentry Demonstrator. Nation: France. Agency: Arianespace. Program: ISS. Class: Technology. Type: Navigation technology satellite. Spacecraft: ARD. COSPAR: 1998-059S. The ARD was an 80 percent scale model of the Apollo Command Module, and a technology test for a possible International Space Station Crew Rescue Vehicle. Equipment included a TDRS satellite communications system; a GPS navigation system; 7 DASA 40 kgf hydrazine attitude control thrusters; a 2.8 m diameter heat shield; three 23 metre diameter parachutes, and a SARSAT recovery beacon. The ARD separated from the Ariane EPS upper stage at 12 minutes 2 seconds after launch. ARD and the EPC stage manoeuvred into a 1 km x 830 km orbit, guaranteeing re-entry at the end of the first orbit. The spacecraft splashed down in the Pacific at 3.69 degrees N, 153.35 degrees W, and was successfully recovered by the French Navy.

1999 October 21 - .
  • ISS Status Report: ISS 99-40 - . Nation: USA. Program: ISS. Flight: ISS EO-1. Summary: In orbit on the International Space Station activities continue to go smoothly with the focus being on systems checks and command link verification between the two control centers and the orbiting complex.. Additional Details: ISS Status Report: ISS 99-40.

2000 October 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 402-01.
  • GE 6 - . Mass: 3,909 kg (8,617 lb). Nation: USA. Agency: GE Americom. Manufacturer: Lockheed. Program: Americom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 26580 . COSPAR: 2000-067A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Communications satellite. Stationed at 72 deg W. The GE 6 was a Lockheed Martin A2100 series satellite with a mass of 3552 kg at launch and 1900 kg dry. It was to provide broadcast and data services in North America. The DM3 upper stage made two burns and placed the GE 6 in a 5850 x 35726 km x 18.7 deg intermediate transfer orbit at 0441 UTC on October 22. Positioned in geosynchronous orbit at 72 deg W in 2000. As of 3 September 2001 located at 72.01 deg W drifting at 0.008 deg W per day. As of 2007 Mar 11 located at 72.00W drifting at 0.005W degrees per day.

2000 October 21 - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL.
  • Thuraya 1 - . Payload: Thuraya 1A. Mass: 5,108 kg (11,261 lb). Nation: UAE. Agency: Thuraya. Manufacturer: El Segundo. Program: Thuraya. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 26578 . COSPAR: 2000-066A. Apogee: 35,808 km (22,250 mi). Perigee: 35,764 km (22,222 mi). Inclination: 5.2000 deg. Period: 1,436.10 min. Mobile Communications satellite. Launch delayed from September 18 and October 19. Stationed at 44 deg E. The first Boeing GEM satellite, Thuraya 1, was built by Boeing/El Segundo (formerly Hughes). It was based on the HS-702 design but featured a large 12-m diameter truss antenna for L-band mobile telephone service. Launch mass of Thuraya was 5108 kg; dry mass probably around 3000 kg. The satellite was to be delivered after on orbit testing to Etisalat, the Emirates Telecom Corp of Abu Dhabi, and its Thuraya Satellite subsidiary. Thuraya was launched from the Odyssey platform in the Pacific Ocean positioned on the equator at 154 deg W. The two-stage Yuzhnoe Zenit core delivered Thuraya and its Energiya Blok DM-SL upper stage to a -2212 x 182 km suborbital trajectory. The first DM-SL burn placed the stack in a 180 x 200 km x 6.3 deg parking orbit at 0604 GMT; a second burn at 0733 GMTput Thuraya in a 210 x 35891 km x 6.3 deg geostationary transfer orbit. A later depletion burn lowered the DM-SL stage perigee to 180 km, as burns by Thuraya's liquid engine raised it towards geosynchronous orbit. Positioned in geosynchronous orbit at 44 deg E in 2000. As of 5 September 2001 located at 44.22 deg E drifting at 0.003 deg E per day. As of 2007 Mar 11 located at 98.57E drifting at 0.007W degrees per day.

2001 October 21 - . 08:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U 672.
  • Soyuz TM-33 - . Call Sign: Derbent. Crew: Afanasyev; Kozeyev; Andre-Deshays. Payload: Soyuz TM 11F732 s/n 207. Mass: 6,750 kg (14,880 lb). Nation: Russia. Related Persons: Afanasyev; Kozeyev; Andre-Deshays. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: ISS EP-2. Spacecraft: Soyuz TM. Duration: 195.79 days. Decay Date: 2002-05-05 . USAF Sat Cat: 26955 . COSPAR: 2001-048A. Apogee: 397 km (246 mi). Perigee: 386 km (239 mi). Inclination: 51.6000 deg. Period: 92.40 min. Soyuz TM-33, an ISS lifeboat, carried two Russian and one French cosmonaut to the International Space Station (ISS). It docked with the ISS at 10:00 UT on 23 October. This new crew spent eight days on the ISS, and returned on the older Soyuz TM-32 at 03:59 UT on 31 October. The new Soyuz was to remain docked as a lifeboat craft for the long-term ISS crew of three (two Russian and one American) astronauts. On May 5, 2002, after a week aboard the station, the visting Soyuz TM-34 crew moved to the old Soyuz TM-33, docked at the Pirs port. They undocked at 0031:08 UTC on May 5, leaving the EO-4 crew of Onufrienko, Walz and Bursch with the new Soyuz TM-34 as their rescue vehicle. Soyuz TM-33 made its deorbit burn at 0257 UTC and landed successfully at 0352 UTC 25 km SE of Arkalyk.

2003 October 21 - . 03:16 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-6 (72).
  • ZY-1-2 (CBERS-2) - . Payload: Zi Yuan 1B. Mass: 1,500 kg (3,300 lb). Nation: China. Agency: CAS. Class: Earth. Type: Earth resources satellite. Spacecraft: ZY. USAF Sat Cat: 28057 . COSPAR: 2003-049A. Apogee: 750 km (460 mi). Perigee: 731 km (454 mi). Inclination: 98.5000 deg. Period: 99.60 min. Summary: Delayed from late 2001, September 3 2002, March 14 and September 2003. Second China-Brazil Earth Resources Satellite (CBERS 2)..
  • CX-1 - . Payload: Chuang Xin 1. Nation: China. Agency: CAS. Class: Technology. Type: Communications technology satellite. Spacecraft: CX-1. USAF Sat Cat: 28058 . COSPAR: 2003-049B. Apogee: 759 km (471 mi). Perigee: 686 km (426 mi). Inclination: 98.5000 deg. Period: 99.20 min. Chuangxin-1 (or Innovation-1) was China's first experimental small satellite for store-and-forward short message data communications in low Earth orbit. With a mass less than 100 kg, the Chuangxin-1 was developed in light of national strategic demands. Starting from 1999 with support of the national Knowledge Innovation Program of the Chinese Academy of Sciences (CAS), the project was carried out jointly by researchers from the CAS Shanghai Institute of Microsystem Information Technology and the CAS Shanghai Institute of Technical Physics. The satellite used spread spectrum communication and subsystems included a communication transponder, onboard computer, attitude control, energy source, thermal control, and structure. The mission was to demonstrate data communications for such sectors as traffic and transportation, environment protection, oil and gas transportation, flood and drought control, detection of forest fire and earthquake monitoring.

2005 October 21 - .
  • International Space Station Status Report #05-52 - . Nation: USA. Related Persons: Tokarev; McArthur. Program: ISS. Flight: ISS EO-11; ISS EO-12. Growing increasingly familiar with their microgravity home and laboratory in space, the 12th international space station crew turned its attention to experiment work, began preparations for the first space station-based spacewalk using U.S. suits since 2003 and captured spectacular images and video of the latest tropical cyclone in the Atlantic basin, Hurricane Wilma. Additional Details: International Space Station Status Report #05-52.

2007 October 21 - . 10:36 GMT - .
2010 October 21 - . 17:00 GMT - . Launch Site: San Nicolas. LV Family: Black Brant. Launch Vehicle: Black Brant 9.
  • NASA 36.230DR - . Nation: USA. Agency: MDA. Apogee: 100 km (60 mi). Summary: ABM target..

2011 October 21 - . 10:30 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELS. LV Family: R-7. Launch Vehicle: Soyuz-2-1B.
  • Galileo-PFM - . Nation: Europe. Class: Navigation. Type: Navigation satellite. Spacecraft: Galileo Navsat. USAF Sat Cat: 37846 . COSPAR: 2011-060A. Apogee: 23,307 km (14,482 mi). Perigee: 23,234 km (14,436 mi). Inclination: 54.7000 deg. Period: 846.80 min. Summary: First Galileo navigation satellites launched to establish an autonomous European navigation satellite constellation. First Soyuz booster launch from the new Ensemble de Lancement Soyuz pad in Kourou..
  • Galileo-FM2 - . Nation: Europe. Class: Navigation. Type: Navigation satellite. Spacecraft: Galileo Navsat. USAF Sat Cat: 37847 . COSPAR: 2011-060B. Apogee: 23,274 km (14,461 mi). Perigee: 23,228 km (14,433 mi). Inclination: 54.7000 deg. Period: 845.90 min.

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