Encyclopedia Astronautica
September 01


September 01 Chronology


1931 September 1 - .
  • Birth of Allen Vinzant - . Nation: USA. Summary: American Chief engineer for interfacing the Centaur upper stage with the Titan 4 launch vehicle..

1936 September 1 - .
  • Tsien Hsue-shen enters CalTech - . Nation: China. Related Persons: Goddard; Tsien; von Karman. Program: Long March. Tsien Hsue-shen, at the urging of Theodore von Karman, begins graduate studies at the California Institute of Technology. He will continue there for nearly twenty years, first as a student, finally as the Goddard Professor, becoming one of the leading rocket scientists in the United States.

1941 September 1 - . Launch Vehicle: Me-163.
  • Me-163A first flight. - . Nation: Germany. Messerschmitt Me-163A powered by "cold" H. Walther rocket successfully flown at Augsburg, Germany, development of which had begun in 1937, but "cold" engine proved unreliable. Flights were also made in October which reached speeds of 1,003 km/hr, or Mach 0.85.

1944 September 1 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P10. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-225.
1945 September 1 - . LV Family: V-2. Launch Vehicle: V-2.
  • Von Braun in America - . Nation: Germany. Related Persons: von Braun. Summary: Von Braun and a small contingent fly to Fort Bliss, Texas. Over 100 Peenemuende rocket engineers will follow by sea..

1948 September 1 - . Launch Site: Wallops Island. LV Family: HVAR. Launch Vehicle: HVAR FFAR.
  • Rascal Model test flight - . Nation: USA. Agency: NASA. Apogee: 5.00 km (3.10 mi).

1951 September 1 - . LV Family: Atlas. Launch Vehicle: Atlas A.
  • Atlas project to concentrate on ballistic missile. - . Nation: USA. Summary: MX-1593 glide missile cancelled. USAF directed all work in Project MX-1593 (Atlas) be for development of a rocket-powered ballistic missile..

1952 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-2. Launch Vehicle: R-2. LV Configuration: R-2 KT-13.
  • Third series controlled test launch - . Nation: USSR. Agency: Korolev. Apogee: 150 km (90 mi).

1953 September 1 - . 05:05 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee XASR-SC-2. LV Configuration: Aerobee XASR-SC-2 SC 32.
  • Grenades Aeronomy mission - . Nation: USA. Agency: USA. Apogee: 108 km (67 mi). Summary: Density research. Launched at 2205 local time. Reached 107.8 km..

1954 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5.
  • Phase 3 state trials launch - . Nation: USSR. Agency: Korolev. Apogee: 300 km (180 mi).

1954 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5.
  • Phase 3 state trials launch - . Nation: USSR. Agency: Korolev. Apogee: 300 km (180 mi).

1954 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5.
  • Phase 3 state trials launch - . Nation: USSR. Agency: Korolev. Apogee: 300 km (180 mi).

1955 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5M.
  • PI state trials launch - . Nation: USSR. Agency: Korolev. Apogee: 500 km (310 mi).

1955 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5M.
  • Test mission - . Nation: USSR. Agency: Korolev. Apogee: 500 km (310 mi).

1955 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5M.
  • Test mission - . Nation: USSR. Agency: Korolev. Apogee: 500 km (310 mi).

1957 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar VLAD. Launch Vehicle: Burya. LV Configuration: Burya 2/1. FAILURE: Premature release of the jet vanes - missile cleared the launch tower, then arced over and crashed.
  • Burya flight 1 - . Nation: USSR. Apogee: 0 km ( mi). Objective was limited to test of operation of first stage boosters. After launch, there was a premature release of the jet vanes. The missile cleared the launch tower, then immediately arced over and crashed with a huge explosion within sight of the launch pad.

1957 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: Kosmos 2. Launch Vehicle: R-12. LV Configuration: R-12 63M No. 7? LKI-7.
  • Test mission - . Nation: USSR. Agency: MVS. Apogee: 402 km (249 mi).

1957 September 1 - . 22:28 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee Hi. LV Configuration: Aerobee Hi AM4.001.
  • Ion probe Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 160 km (90 mi).

1958 September 1 - .
  • Tsien enters Congress - . Nation: China. Related Persons: Tsien. Summary: Tsien was elected Deputy of Guangdong Province to the National People's Congress..

1958 September 1 - . LV Family: Saturn I. Launch Vehicle: Saturn I.
  • Redstone Arsenal begins Saturn I design studies. - . Nation: USA. Related Persons: von Braun. Program: Apollo. Summary: Saturn design studies authorized to proceed at Redstone Arsenal for development of 1.5-million-pound-thrust cluster first stage..

1959 September 1 - .
  • McDonnell report on a modified Mercury capsule to explore problems of space flight. - . Nation: USA. Spacecraft: Mercury Mark I. McDonnell Aircraft Corporation, St. Louis, Missouri, issued a report on the company's studies using a modified Mercury capsule to explore some problems of space flight beyond the initial manned exploration of space through Mercury. The 300-page report discussed six follow-on experiments: touchdown control, maneuver in orbit, self-contained guidance, 14-day mission, manned reconnaissance, and lunar-orbit reentry. These were more in the nature of technically supported suggestions than firm proposals, but all six experiments could be conducted with practical modifications of Mercury capsules.

1959 September 1 - .
  • Mercury spacecraft modified to withstand lunar reentry conditions - . Nation: USA. Program: Apollo. Spacecraft: Mercury. McDonnell Aircraft Corporation reported to NASA the results of several company-funded studies of follow-on experiments using Mercury spacecraft with heatshields modified to withstand lunar reentry conditions. In one experiment, a Centaur booster would accelerate a Mercury spacecraft plus a third stage into an eccentric earth orbit with an apogee of about 1,200 miles, so that the capsule would reenter at an angle similar to that required for reentry from lunar orbit. The third stage would then fire, boosting the spacecraft to a speed of 36,000 feet per second as it reentered the atmosphere.

1959 September 1 - . Launch Site: Vandenberg. LV Family: Atlas. Launch Vehicle: Atlas D.
  • Atlas D ICBM operational. - . Nation: USA. Summary: USAF Atlas ICBM officially declared operational and taken over by the Strategic Air Command, at Vandenberg AFB..

1959 September 1 - . 01:01 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LC-A. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp NN8.74CF.
  • Solar mission - . Nation: USA. Agency: USN. Apogee: 200 km (120 mi).

1959 September 1 - . 19:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LC-A. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp NN8.75CF.
  • Ionosphere / plasma / solar mission - . Nation: USA. Agency: USN. Apogee: 210 km (130 mi).

1960 September 1 - .
  • Apollo Project Office formed - . Nation: USA. Related Persons: Faget. Program: Apollo. In an organizational change within STG, Maxime A. Faget was appointed Chief of the Flight Systems Division and Robert O. Piland was named Assistant Chief for Advanced Projects. The Apollo Project Office was formed with Piland as Head of the Office; members included John B. Lee, J. Thomas Markley, William W. Petynia,and H. Kurt Strass.

1960 September 1 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA3. LV Family: R-2. Launch Vehicle: R-2.
  • - . Nation: China. Agency: PRC. Apogee: 100 km (60 mi). Summary: The rocket was built in the Soviet Union but used Chinese propellants. This launch took place just a month after all Soviet experts were withdrawn from China..

1960 September 1 - . Launch Site: Shijiedu. LV Family: T-7. Launch Vehicle: T-7.
  • Test mission - . Nation: China. Agency: Shanghai. Apogee: 60 km (37 mi). Summary: First launch of the all-up missile..

1961 September 1 - .
1961 September 1 - . Launch Site: Baikonur. LV Family: R-16. Launch Vehicle: R-16.
  • New ICBM tests announced. - . Nation: USSR. Summary: U.S.S.R. announced that it would launch a series of "more powerful and improved rockets. (Article in Red Star timed to coincide with first firing of new rocket series in the Pacific.).

1962 September 1 - . 02:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78. LV Configuration: Molniya 8K78 T103-13. FAILURE: At T+ 61 min 30 sec the fuel valve did not open.; the ignition command was blocked from going to the main engine of Stage 4.. Failed Stage: 3.
  • Sputnik 20 - . Payload: 2MV-1 s/n 2. Mass: 6,500 kg (14,300 lb). Nation: USSR. Agency: RVSN. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft: Mars 2MV-1. Decay Date: 1962-09-06 . USAF Sat Cat: 381 . COSPAR: 1962-A-Tau-1. Apogee: 246 km (152 mi). Perigee: 185 km (114 mi). Inclination: 64.7000 deg. Period: 88.80 min.

1962 September 1 - . 20:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1E. LV Family: Delta. Launch Vehicle: Thor Agena B. LV Configuration: Thor Agena B 348 / Agena B 1132.
  • KH-5 9042A - . Payload: KH-5 s/n 9042A/Agena B 1132. Mass: 1,150 kg (2,530 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-5. Decay Date: 1964-10-26 . USAF Sat Cat: 385 . COSPAR: 1962-A-Upsilon-1. Apogee: 639 km (397 mi). Perigee: 293 km (182 mi). Inclination: 82.8000 deg. Period: 94.00 min. Summary: KH-5. Mission failed. Parachute shrouds parted during air catch, capsule sank. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A)..
  • SRV 600 - . Nation: USA. Agency: USAF. Spacecraft: KH-5. COSPAR: 1962-A-Upsilon-x.

1963 September 1 - . Launch Site: Baikonur. Launch Complex: Baikonur LC110L. LV Family: N1. Launch Vehicle: N1.
  • Construction begins of N1 launch complex - . Nation: USSR. Program: Lunar L3.

1963 September 1 - . Launch Site: Sary Shagan. Launch Complex: Sary Shagan LC6. LV Family: A-35. Launch Vehicle: A-350Zh. LV Configuration: A-350Zh 6TYa F1.
  • Test mission - . Nation: USSR. Agency: PKO. Apogee: 100 km (60 mi).

1964 September 1 - . Launch Site: Baikonur. Launch Complex: Baikonur LC110L. LV Family: N1. Launch Vehicle: N1.
  • Construction start of N1 launch complex 110 east - . Nation: USSR. Program: Lunar L3.

1964 September 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 668.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1964 September 1 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC20. LV Family: Titan. Launch Vehicle: Titan 3A. LV Configuration: Titan IIIA 3A-2. FAILURE: Transtage pressurization failure caused premature shutdown.. Failed Stage: 3.
  • Titan 3A Transtage 1 - . Payload: Transtage 2. Nation: USA. Agency: USAF. Decay Date: 1964-09-02 . COSPAR: F640901A.

1964 September 1 - . 09:19 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 7C. LV Configuration: Skylark-7C SL137.
  • Ozone distribution Aeronomy mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 212 km (131 mi).

1965 September 1 - .
  • Apollo LEM ascent engine exploded during firings - . Nation: USA. Program: Apollo. Spacecraft: Apollo LM; LM Ascent Propulsion. A LEM ascent engine exploded during altitude firings at Arnold Engineering Development Center (AEDC). In subsequent investigations, Bell Aerosystems researchers concluded that the failure probably resulted from raw propellants being accidentally forced into the engine at the end of the second run, thus damaging the injector. Additional Details: Apollo LEM ascent engine exploded during firings.

1965 September 1 - .
  • Impact tests with Apollo boilerplate 28 - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Heat Shield. North American conducted another in their series of impact tests with boilerplate 28. This drop tested the toroidal section of the spacecraft (heatshield and equipment bay structure) in impact at high angle and maximum horizontal velocity. The spacecraft suffered no visible damage. Some water leaked into the vehicle, but this was blamed on the boilerplate structure itself and the apex-down attitude after impact.

1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-15. Launch Vehicle: RT-15.
  • Test mission - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1965 September 1 - . 11:17 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.213UI.
  • MIP 1 Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 150 km (90 mi).

1966 September 1 - . LV Family: N1. Launch Vehicle: N1.
  • N1-L3 manned landing profile approved. - . Nation: USSR. Spacecraft: LK; Soyuz 7K-LOK. Summary: Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On approval of the N1-L3 mission profile' was issued..

1966 September 1 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 656. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-386.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 September 1 - . Launch Site: Barking Sands. LV Family: Strypi. Launch Vehicle: Strypi IV.
  • HALBERD re-entry vehicle test flight - . Nation: USA. Agency: Sandia. Apogee: 200 km (120 mi).

1966 September 1 - . Launch Site: Green River. Launch Complex: Green River Pad 2. LV Family: Athena RTV. Launch Vehicle: Athena RTV. LV Configuration: Athena D029.
  • USAF D029 re-entry vehicle test flight - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1966 September 1 - . 18:58 GMT - . Launch Site: Fort Churchill. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.18UE.
  • Auroral radiation Plasma mission - . Nation: USA. Agency: NASA. Apogee: 242 km (150 mi).

1967 September 1 - .
  • S-IVB Orbital Workshop mockup returned for a number of design changes. - . Nation: USA. Spacecraft: Orbital Workshop. MSFC returned a McDonnell Douglas-built S-IVB Orbital Workshop mockup to the contractor's Space Systems Center in Huntington Beach, California, for incorporation of a number of design changes. Following modification, the mockup would represent the S IVB stage as a manned space laboratory designed for use in the AAP. The design changes included relocation of a floor separating two sections of the stage's liquid hydrogen tank, addition of a ceiling and other fixtures, and relocation of some of the experiment stations.

1967 September 1 - . Launch Site: Sary Shagan. Launch Complex: Sary Shagan LC6. LV Family: A-35. Launch Vehicle: A-350Zh.
  • Phase 1 state trials flight - . Nation: USSR. Agency: PKO. Apogee: 300 km (180 mi).

1967 September 1 - . 10:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Voskhod 11A57. FAILURE: Failure of Block I stage at 296 seconds. Remnants of spacecraft and stage fell near Novaya Zemlya.. Failed Stage: 2.
  • Zenit-2 11F61 s/n 51 - . Payload: Zenit-2 11F61 s/n 51. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: RVSN. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Decay Date: 1967-09-01 . COSPAR: F670901A. Summary: Area survey photo reconnaissance satellite..

1968 September 1 - . 18:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 1442.
  • ST (Partial fuel) - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1969 September 1 - . LV Family: N1; UR-700.
  • Kamanin lists the reasons the Soviets have lost the moon race. - . Nation: USSR. Related Persons: Mishin; Ustinov; Smirnov; Korolev; Keldysh; Feoktistov; Gagarin. Program: Apollo; Lunar L1; Lunar L3. Spacecraft: Soyuz 7K-OK; Soyuz 7K-LOK; Soyuz 7K-L1. The Americans were able to pull equal in the race during their Gemini programme, then ahead with Apollo. The Soviet Union is now four to five years behind. Kamanin's accounting:

    • No qualified Soviet government leadership in space research (Ustinov and Smirnov are a parody of proper management). They operate without rhyme or reason or plan. There is no single direction, no disciplined execution when a decision is finally made
    • Korolev, Keldysh, Mishin, and Feoktistov are all dedicated to automated spacecraft - 'over-automation'
    • Korolev and MIshin's rejection of Glushko's engines, and the leadership's rejection of the UR-700 as an alternative
    • Ustinov and Smirnov's cancellation of the 18 day Voskhod 3 mission, even though the crews had been trained, and the associated pressure on development of Soyuz. This resulted in Soyuz being flown before it was mature, resulting in the death of Komarov and an 18 month delay in manned flights
    • Death of Korolev and Gagarin both badly affected morale
    • Making Mishin head of TsKBEM was a huge mistake. Mishin cannot cope with the huge number of space and missile projects assigned to his bureau

1969 September 1 - .
  • Soviets study NASA's ambitious plans - . Nation: USSR. Spacecraft: LESA Shelter; LLV. NASA gave the US President a 130-page programme outlining plans for America's future space programme. The thing read to the Soviets like a science fiction novel, with reusable space ferries, huge orbital stations and lunar bases, nuclear rocket stages, and manned Mars expeditions. There was no way the Soviet Union could compete with such a programme -- and that was leaving unconsidered the massive American military space progamme. Additional Details: Soviets study NASA's ambitious plans.

1970 September 1 - . 01:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC13. LV Family: Atlas. Launch Vehicle: Atlas Agena D SLV-3A. LV Configuration: SLV-3A Agena D 5203A / Agena D 2803.
  • Canyon 3 - . Payload: Canyon 3 / Agena D / OPS 7329. Mass: 700 kg (1,540 lb). Nation: USA. Agency: USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Canyon. USAF Sat Cat: 4510 . COSPAR: 1970-069A. Apogee: 39,855 km (24,764 mi). Perigee: 31,947 km (19,850 mi). Inclination: 10.3000 deg. Period: 1,441.90 min. Summary: Positioned in geosynchronous orbit over the Indian Ocean. Last known longitude (31 December 1970) 99.01 deg W drifting at 1.490 deg W per day..

1970 September 1 - . 20:10 GMT - . Launch Site: Wallops Island. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.52UA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 800 km (490 mi).

1971 September 1 - .
  • Soviet-Indian collaboration to build a new satellite. - . Nation: USSR. Spacecraft: Bhaskara. Summary: Decree 'On co-operation to build an Indian satellite' was issued..

1971 September 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 74F.
  • ABRES LAR-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1971 September 1 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 616. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 September 1 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 616. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 September 1 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 616. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 September 1 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 616. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 September 1 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 616. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 September 1 - . 02:10 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 10. LV Configuration: Kappa 10 K-10-6.
  • Solar ultraviolet Solar ultraviolet mission - . Nation: Japan. Agency: ISAS. Apogee: 228 km (141 mi).

1972 September 1 - .
  • L3 terminated. - . Nation: USSR. Spacecraft: LK; Soyuz 7K-LOK. Summary: Decree 'On termination of production work on the L3' was issued..

1972 September 1 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 September 1 - . Launch Site: Plesetsk. Launch Vehicle: Temp-2S.
  • Test mission - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1972 September 1 - . 04:10 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170A. LV Configuration: Aerobee 170A NASA 13.47UL.
  • JHU UVT F7 Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 159 km (98 mi).

1972 September 1 - . 17:44 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 24B. LV Configuration: Titan 24B 24B-5 (3B-39).
  • OPS 8888 - . Payload: KH-8 no. 36 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA. Agency: NRO; USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-8. Decay Date: 1972-09-30 . USAF Sat Cat: 6172 . COSPAR: 1972-068A. Apogee: 381 km (236 mi). Perigee: 142 km (88 mi). Inclination: 110.4000 deg. Period: 89.70 min. Summary: KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

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

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

1974 September 1 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1974 September 1 - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. LV Family: Lambda. Launch Vehicle: Lambda 4SC. LV Configuration: Lambda 4SC L-4SC-3.
  • TVC test - . Nation: Japan. Agency: ISAS. Apogee: 1,500 km (900 mi).

1975 September 1 - . Launch Site: Fort Churchill. LV Family: Loki. Launch Vehicle: Super Loki.
  • Meteorological mission - . Nation: USA. Agency: MRN. Apogee: 75 km (46 mi).

1976 September 1 - . 00:00 GMT - . Launch Site: Syowa Base. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210JA-25.
  • E / B / ne Aurora mission - . Nation: Japan. Agency: NIPR. Apogee: 125 km (77 mi).

1976 September 1 - . 03:23 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Molniya 8K78M. FAILURE: Fourth stage failure.. Failed Stage: 3.
  • Cosmos 853 - . Payload: Molniya-2 s/n 26. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-2. Decay Date: 1976-12-31 . USAF Sat Cat: 9398 . COSPAR: 1976-088A. Apogee: 461 km (286 mi). Perigee: 243 km (150 mi). Inclination: 62.8000 deg. Period: 91.60 min. Summary: Failed Molniya..

1976 September 1 - . 21:14 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout D-1. LV Configuration: Scout D-1 S197C.
  • TIP 3 - . Payload: Triad 3 (TIP 3). Mass: 94 kg (207 lb). Nation: USA. Agency: USN. Program: Transit. Class: Navigation. Type: Navigation satellite. Spacecraft: TIP. Decay Date: 1981-05-30 . USAF Sat Cat: 9403 . COSPAR: 1976-089A. Apogee: 789 km (490 mi). Perigee: 345 km (214 mi). Inclination: 90.3000 deg. Period: 95.90 min. Summary: Prototype of improved Transit satellite. Also tested pulsed plasma engine..

1977 September 1 - . 21:34 GMT - . Launch Site: Barking Sands. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 88 km (54 mi).

1978 September 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1979 September 1 - .
1979 September 1 - . 04:16 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3TK P-5.
  • Chevaline warhead test launch - . Nation: UK. Agency: RN. Apogee: 1,000 km (600 mi).

1980 September 1 - . Launch Site: Barking Sands. LV Family: Strypi. Launch Vehicle: Strypi. LV Configuration: Strypi SWERVE II-1.
  • Re-entry Vehicle test - . Nation: USA. Agency: Sandia. Apogee: 200 km (120 mi).

1980 September 1 - . Launch Site: Barking Sands. LV Family: Strypi. Launch Vehicle: Strypi. LV Configuration: Strypi SWERVE II-2.
  • Re-entry Vehicle test - . Nation: USA. Agency: Sandia. Apogee: 200 km (120 mi).

1981 September 1 - .
  • Cosmonaut Bui Thanh Liem dies at age of 32 -- Crash of MiG-21 fighter. - . Nation: USSR. Related Persons: Liem. Summary: Vietnamese pilot cosmonaut, 1979-1980. Graduated from Gagarin Military Academy, Monino, 1978 Captain and fighter pilot, Vietnam Air Force. Flew many combat missions during the Vietnam-war. Continued service in Vietnamese Air Force..

1982 September 1 - .
  • USAF activated Space Command under General James Hartinger's leadership. - . Nation: USA.

1982 September 1 - .
  • DoD Astronaut Training Group 2 selected. - . Nation: USA. Related Persons: Armor; Booen; Holder; James; Jones, Charles; LaComb; Mantz; Odle; Pailes; Puz; Roberts; Sponable; Thompson, David; Yeakel. The group was selected to provide shuttle manned spaceflight engineers to operate military payloads.. Qualifications: USAF officers with bachelor's degree in science or engineering; four years experience in flying or space-related activities. Vision minimum 20/150 uncorrected, correctable to 20/20. Maximum sitting blood pressure of 140/90. Height between 150 and 193 cm.. 14 were selected from 63 candidates.

1982 September 1 - . 09:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1403 - . 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: 1982-09-15 . USAF Sat Cat: 13448 . COSPAR: 1982-085A. Apogee: 353 km (219 mi). Perigee: 205 km (127 mi). Inclination: 70.4000 deg. Period: 90.10 min. Summary: Photo surveillance; returned film capsule..

1982 September 1 - . 11:40 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1404 - . 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: 1982-09-15 . USAF Sat Cat: 13449 . COSPAR: 1982-086A. Apogee: 354 km (219 mi). Perigee: 196 km (121 mi). Inclination: 72.8000 deg. Period: 90.00 min. Summary: Photo surveillance; returned film capsule..

1983 September 1 - . 22:40 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Taurus Tomahawk Nike. LV Configuration: Taurus Nike Tomahawk NASA 12.39WT. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1984 September 1 - . Launch Site: Gitdaeryung. LV Family: R-17. Launch Vehicle: Hwasong 5.
1984 September 1 - . Launch Site: Gitdaeryung. LV Family: R-17. Launch Vehicle: Hwasong 5.
1985 September 1 - .
1985 September 1 - .
  • DoD Astronaut Training Group 3 selected. - . Nation: USA. Related Persons: Carretto; Crombie; DeArmond; Staib; Tittle. The group was selected to provide shuttle manned spaceflight engineers to operate military payloads.. Qualifications: USAF officers with bachelor's degree in science or engineering; four years experience in flying or space-related activities. Vision minimum 20/150 uncorrected, correctable to 20/20. Maximum sitting blood pressure of 140/90. Height between 150 and 193 cm.. 5 were selected from 160 candidates.

1986 September 1 - . LV Family: Energia. Launch Vehicle: Energia.
  • Second Energia full thrust test - . Nation: USSR. Program: Buran. Spacecraft: Buran. Summary: The second engine test was a complete success, the engine running for 390 seconds. This test required the entire city of Leninsk to be without water for ten days in order to accumulate enough water for the UKSS cooling system..

1986 September 1 - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: DELTA2. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1987 September 1 - . 07:58 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • IPMS - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1988 September 1 - . LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: STS-51-K.
  • STS-51-K (cancelled) - . Payload: Spacelab-D1 . Nation: USA. Program: STS. Flight: STS-51-K. Spacecraft: Challenger. Summary: Planned Spacelab-D1 shuttle mission. Cancelled after Challenger disaster. No crew selected; renamed STS-61A.

1989 September 1 - . 19:40 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1990 September 1 - . 12:05 GMT - . Launch Site: Thumba. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 80 km (49 mi).

1991 September 1 - . Launch Site: Atlantic Ocean. Launch Pad: 15.0 N x 65.0 W. Launch Platform: ZUB. LV Family: MR-12. Launch Vehicle: MR-20.
  • - . Nation: USSR. Apogee: 250 km (150 mi).

1992 September 1 - . 01:00 GMT - . Launch Site: White Sands. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.92UU.
  • CWAS 26 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1993 September 1 - . Launch Site: Anhueng. LV Family: KSR. Launch Vehicle: KSR-I. LV Configuration: KSR-I-2.
  • Ozone profile mission - . Nation: Korea South. Agency: KARI. Apogee: 49 km (30 mi). Summary: Ultraviolet radiometer to measure vertical ozone distribution in the stratosphere over the Korean peninsula. Rocket performance also monitored..

1997 September 1 - . 14:00 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-2C/SD. LV Configuration: Chang Zheng 2C-III/SD CZ2C-15 (47).
  • Iridium - . Payload: Iridium s/n MFS 1. Mass: 689 kg (1,518 lb). Nation: USA. Agency: Iridium. Manufacturer: Lockheed; Motorola. Program: Iridium. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 24925 . COSPAR: 1997-048A. Apogee: 633 km (393 mi). Perigee: 620 km (380 mi). Inclination: 86.3400 deg. Period: 97.25 min. Summary: Plane 5. Ascending node 271.9 degrees. Dummy satellite..
  • Iridium - . Payload: Iridium s/n MFS 2. Mass: 689 kg (1,518 lb). Nation: USA. Agency: Iridium. Manufacturer: Lockheed; Motorola. Program: Iridium. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 24926 . COSPAR: 1997-048B. Apogee: 634 km (393 mi). Perigee: 620 km (380 mi). Inclination: 86.3400 deg. Period: 97.26 min. Summary: Plane 5. Ascending node 272 degrees. Dummy satellite..

1998 September 1 - . Launch Site: Mojave.
  • Proteus roll-out. - . Nation: USA. Program: X-Prize. Spacecraft: SpaceShipOne. Summary: Scaled Composites (Mojave, California, USA) rolls out and tests Proteus aircraft, predecessor of White Knight carrier-launcher for Tier One/SpaceShipOne..

1999 September 1 - .
2000 September 1 - . Launch Site: Hama-Allepo. LV Family: R-17. Launch Vehicle: R-17. LV Configuration: Scud D.
  • Test mission - . Nation: Syria. Agency: SYMC. Apogee: 150 km (90 mi).

2000 September 1 - . 03:25 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-3 (62).
  • ZY-2 - . Payload: Zi Yuan 2. Nation: China. Agency: SISE. Manufacturer: CAST. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: ZY. USAF Sat Cat: 26481 . COSPAR: 2000-050A. Apogee: 501 km (311 mi). Perigee: 489 km (303 mi). Inclination: 97.4000 deg. Period: 94.43 min. The ZY-2 (Ziyuan-2 ('Resource-2'), while disguised as a civilian earth monitoring system, was actually code-named Jianbing-3 and was China's first high-resolution military imaging satellite. The cover story of the official Xinhua news agency was that the civilian remote sensing system would be used primarily in territorial surveying, city planning, crop yield assessment, disaster monitoring and space science experimentation. However the satellite was placed at a much lower altitude than the ZY-1 satellite and US intelligence sources indicated that it was a photo-reconnaissance satellite for exclusively military purposes, such as targeting missiles at US and Taiwanese forces. The new satellite was believed to employ digital-imaging technology and to have a resolution of 2 m or less. The satellite was designed and built by the Chinese Academy of Space Technology and was developed indigenously. It was said to be more advanced than earlier sensing satellites and was expected to have an orbital life of two years. The camera provided more than three times the resolution of the ZY-1 earth resources satellite. The Zi Yuan 2 satellite may have used the CBERS Sino-Brazilian bus of the earlier ZY-1. However it was also said to be of new design and demonstrated the capability to maneuver in orbit, adjusting its orbit after launch. In October 2000 Chinese scientists denied that the ZY-2 satellite had a military mission. It was said to be a remote-sensing satellite equipped with CCD cameras and an infrared multispectral scanner that could only identify objects on the ground with a resolution of several dozen meters to 1 km.

2001 September 1 - . 10:35 GMT - . Launch Site: SvalRak. Launch Complex: SvalRak LONG. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A ROFS-22.
  • ROMA Aeronomy mission - . Nation: Germany. Agency: DLR. Apogee: 100 km (60 mi).

2003 September 1 - .
  • Galileo Exits Solar Conjunction - . Nation: USA. Spacecraft: Galileo.

2004 September 1 - . 14:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. LV Family: Loki. Launch Vehicle: Super Loki.
  • Shadow 1B Education mission - . Nation: USA. Agency: FLASPACE. Apogee: 110 km (60 mi).

2005 September 1 - .
2006 September 1 - . 17:22 GMT - . Launch Site: Kodiak. LV Family: Polaris. Launch Vehicle: STARS. LV Configuration: STARS M-8.
  • GMD FTG-02 Target - . Nation: USA. Agency: USA SMDC. Apogee: 1,000 km (600 mi).

2006 September 1 - . 17:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF23. Launch Pad: LF23?. Launch Vehicle: OBV. LV Configuration: OBV 5.
  • FT-2 - . Nation: USA. Agency: OSC; MDA. Apogee: 1,000 km (600 mi).

2010 September 1 - . Launch Site: Point Mugu. LV Family: R-17. Launch Vehicle: R-17. LV Configuration: Scud FMA.
  • RV - . Nation: USA. Agency: MDA. Apogee: 100 km (60 mi). Summary: ABM target..

2011 September 1 - . 13:43 GMT - . Launch Site: Barking Sands. LV Family: Terrier. Launch Vehicle: Terrier Oriole.
  • ARAV - . Nation: USA. Apogee: 150 km (90 mi). Summary: Target for SM-3 Block IB interceptor..
  • Aegis KV - . Nation: USA. Apogee: 150 km (90 mi). Summary: Interceptor mission. First test flight of the Block IB version of the SM-3 missile interceptor. Failed to hit its target..

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