Chronology - Quarter 2 1976 home
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1976 April 1 - 08:05 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Sounding Rocket. LV Configuration: Sergeant IC630.02-1A.
  • ICECAP 76 HIRIS Auroral mission Nation: USA. Agency: DNA/AFCRL. Apogee: 130 km (80 mi). References: 2.
1976 April 1 - 09:28 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Hydac. LV Configuration: HJ Hydac ARPA WS650.27-1.
  • Ballistics test Nation: USA. Agency: ARPA. Apogee: 150 km (90 mi). References: 2.
1976 April 2 -
  • Crew escape system test sled on dock, Downey Nation: USA. Program: STS. References: 15.
1976 April 2 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena Athena D.
  • MSV-1 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1976 April 3 -
  • Complete assembly and deliver MPTA structure Nation: USA. Program: STS. Complete assembly and deliver MPTA structure on dock, Lockheed test site, Palmdale References: 15.
1976 April 6 - 04:14 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-280.
  • Cosmos 812 Nation: USSR. Program: Tselina. Mass: 900 kg (1,980 lb). Class: Sigint. Spacecraft: Tselina-O. Agency: MO SSSR. Perigee: 508 km (315 mi). Apogee: 548 km (340 mi). Inclination: 74.00 deg. Period: 95.20 min. COSPAR: 1976-031A. USAF Sat Cat: 8794. Decay Date: 1980-10-30. Replaced Cosmos 544. Possible ELINT satellite. References: 2, 6.
1976 April 7 - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: MSBS. Model: MSBS M20.
  • Operational test Nation: France. Agency: DMA. Apogee: 600 km (370 mi). References: 2.
1976 April 7 - 13:05 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Meteor 1-24 Nation: USSR. Payload: Meteor M s/n 37. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor M. Agency: MOM. Perigee: 832 km (516 mi). Apogee: 881 km (547 mi). Inclination: 81.30 deg. Period: 102.10 min. COSPAR: 1976-032A. USAF Sat Cat: 8799. Acquisition of meteorological information needed for use by the weather service. References: 2, 6.
1976 April 9 - 08:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 813 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 209 km (129 mi). Apogee: 236 km (146 mi). Inclination: 81.30 deg. Period: 88.90 min. COSPAR: 1976-033A. USAF Sat Cat: 8801. Duration: 12.00 days. Decay Date: 1976-04-21. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1976 April 13 - 17:16 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 814 Nation: USSR. Mass: 1,400 kg (3,000 lb). Class: Military. Type: ASAT. Spacecraft: IS-A. Agency: PKO. Perigee: 118 km (73 mi). Apogee: 480 km (290 mi). Inclination: 65.10 deg. Period: 90.50 min. COSPAR: 1976-034A. USAF Sat Cat: 8806. Decay Date: 1976-04-13. ASAT interceptor. After intercept with target deorbited using on-board engine. References: 2, 6, 272.
1976 April 17 -
  • Closest Ever Flyby of the Sun by Spacecraft (Helios 2) Nation: Germany. Spacecraft: Helios.
1976 April 18 - 23:55 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2B. LV Configuration: Centaure 2B ISRO 5.32.
  • ISRO 5.32 Aeronomy / ionosphere mission Nation: India. Agency: ISRO. Apogee: 152 km (94 mi). References: 2.
1976 April 20 - 20:08 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-18? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 April 20 - 20:09 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-18? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 April 21 - 10:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.49DH.
  • NRL XR X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 202 km (125 mi). References: 2.
1976 April 22 -
  • Body flap on dock, Palmdale, Enterprise (OV-101) Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise. References: 15.
1976 April 22 - 20:46 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2914. LV Configuration: Delta 2914 608/D122.
  • NATO 3A Nation: NATO. Program: NATO. Mass: 310 kg (680 lb). Class: Communications. Type: Military. Spacecraft: NATO 3. Agency: NATO. Perigee: 35,801 km (22,245 mi). Apogee: 36,017 km (22,379 mi). Inclination: 13.30 deg. Period: 1,442.40 min. COSPAR: 1976-035A. USAF Sat Cat: 8808. Completed Operations Date: 1992-12-17. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Atlantic Ocean at 18 deg W in 1976-1982; over the Atlantic Ocean 30 deg W in 1982-1984; over the Atlantic Ocean 50 deg W in 1984-1985; over the Atlantic Ocean at 30 deg W in 1985-1989; over the Americas at 125 deg W in 1989-1991 As of 5 September 2001 located at 4.12 deg E drifting at 1.524 deg W per day. As of 2007 Mar 9 located at 142.00E drifting at 1.522W degrees per day. References: 2, 6.
1976 April 23 - 09:46 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-19? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 April 23 - 09:53 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-19? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 April 25 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena SAMSO-39.
  • ABRES Re-entry Vehicle test Nation: USA. Agency: USAF/Sandia. Apogee: 200 km (120 mi). References: 2.
1976 April 28 - 09:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 815 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 218 km (135 mi). Apogee: 231 km (143 mi). Inclination: 81.30 deg. Period: 89.00 min. COSPAR: 1976-036A. USAF Sat Cat: 8811. Duration: 13.00 days. Decay Date: 1976-05-11. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1976 April 28 - 13:30 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53746-301.
  • Cosmos 816 Nation: USSR. Mass: 950 kg (2,090 lb). Class: Calibration. Spacecraft: Taifun-2. Agency: MO SSSR. Perigee: 453 km (281 mi). Apogee: 566 km (351 mi). Inclination: 65.90 deg. Period: 94.80 min. COSPAR: 1976-037A. USAF Sat Cat: 8812. Decay Date: 1979-11-24. Released 24 Romb radar calibration subsatellites. References: 2, 6.
1976 April 29 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Corella.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 200 km (120 mi). References: 2.
1976 April 30 - 04:35 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk GL A10.001-2.
  • Auroral ions Aeronomy mission Nation: USA. Agency: USAF GL. Apogee: 218 km (135 mi). References: 2.
1976 April 30 - 19:12 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F/MSD. LV Configuration: Atlas F/MSD 59F.
  • NOSS 1 (Whitecloud 1) Nation: USA. Payload: PARCAE 1. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS. Agency: USN. Perigee: 1,092 km (678 mi). Apogee: 1,128 km (700 mi). Inclination: 63.50 deg. Period: 107.50 min. COSPAR: 1976-038A. USAF Sat Cat: 8818. Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE. References: 2, 6, 172, 278.
  • SSU 1 (NOSS 1) Nation: USA. Payload: NOSS-Subsat 1-1. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS-Subsat. Agency: USN. Perigee: 932 km (579 mi). Apogee: 1,284 km (797 mi). Inclination: 63.40 deg. Period: 107.40 min. COSPAR: 1976-038C. USAF Sat Cat: 8835. Deployed from NOSS 1. References: 2, 6, 278.
  • SSU 2 (NOSS 1) Nation: USA. Payload: NOSS-Subsat 1-2. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS-Subsat. Agency: USN. Perigee: 931 km (578 mi). Apogee: 1,286 km (799 mi). Inclination: 63.40 deg. Period: 107.40 min. COSPAR: 1976-038D. USAF Sat Cat: 8836. Deployed from NOSS 1. References: 2, 6, 278.
  • SSU 3 (NOSS 1) Nation: USA. Payload: NOSS-Subsat 1-3. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS-Subsat. Agency: USN. Perigee: 893 km (554 mi). Apogee: 1,324 km (822 mi). Inclination: 63.40 deg. Period: 107.40 min. COSPAR: 1976-038J. USAF Sat Cat: 8884. Deployed from NOSS 1. References: 2, 6, 278.
1976 May 1 - Launch Vehicle: Energia, N1.
  • Plea for revival of N1 project Nation: USSR. Program: Lunar L3. Spacecraft: Buran. The workers on the project put together a letter to the 25th Party Congress, saying that N1 development should continue, and that N1 s/n's 8, 9, and 10 should be flown. The Party did not accept the letter. They had been assured by the leadership that the population of the city of Leninsk, the extensive facilities and housing built for the N1, would all be used for the MKTS Soviet shuttle. Iosifiyan considered the N1 fundamentally flawed, a project that was only approved due to Kremlin politics. References: 367.
1976 May 3 -
  • MPTA-098 proof load test setup Nation: USA. Program: STS. MPTA-098 proof load test setup, Lockheed test site, Palmdale References: 15.
1976 May 4 - 08:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2913. LV Configuration: Delta 2913 609/D123.
  • Lageos Nation: USA. Payload: Lageos 1. Mass: 411 kg (906 lb). Class: Earth. Type: Geodetic. Spacecraft: Lageos. Agency: NASA MSF. Perigee: 5,839 km (3,628 mi). Apogee: 5,947 km (3,695 mi). Inclination: 109.90 deg. Period: 225.50 min. COSPAR: 1976-039A. USAF Sat Cat: 8820. LAGEOS (Laser Geodetic Satellite) was a very dense (high mass-to-area ratio) laser retroreflector satellite which provided a permanent reference point in a very stable orbit for such precision earth-dynamics measurements as crustal motions, regional strains, fault motions, polar motion and earth-rotation variations, solid earth tides, and other kinematic and dynamic parameters associated with earthquake assessment and alleviation. The performance in orbit of LAGEOS was limited only by degradation of the retroreflectors, so many decades of useful life can be expected. The high mass-to-area ratio and the precise, stable (attitude-independent) geometry of the spacecraft, together with the orbit, made this satellite the most precise position reference available. Because it is visible in all parts of the world and has an extended operation life in orbit, LAGEOS can serve as a fundamental standard for decades. Additional Details: Lageos. References: 2, 6.
1976 May 5 - 07:50 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 817 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 173 km (107 mi). Apogee: 324 km (201 mi). Inclination: 65.00 deg. Period: 89.50 min. COSPAR: 1976-040A. USAF Sat Cat: 8823. Duration: 13.00 days. Decay Date: 1976-05-18. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1976 May 6 - 11:44 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P186H.
  • Mass spectrometer Ionosphere mission Nation: UK. Agency: SRC. Apogee: 149 km (92 mi). References: 2.
1976 May 6 - 12:21 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P115H.
  • Faraday rotation Ionosphere mission Nation: UK. Agency: SRC. Apogee: 137 km (85 mi). References: 2.
1976 May 11 - 08:55 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.38GH.
  • CIT Cyg X-1 X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 175 km (108 mi). References: 2.
1976 May 11 - 17:08 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200. LV Configuration: Aerobee 200 NASA 26.45CS.
  • Solar mission Nation: USA. Agency: NASA. Apogee: 248 km (154 mi). References: 2.
1976 May 12 - 10:50 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7 AC. LV Configuration: Skylark 7 AC SL1115.
  • X-ray Telescope X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 231 km (143 mi). References: 2.
1976 May 12 - 17:57 GMT - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Molniya 3-05 Nation: USSR. Program: Molniya. Payload: Molniya-3 s/n 16. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-3. Agency: MOM. Perigee: 93 km (57 mi). Apogee: 37,589 km (23,356 mi). Inclination: 62.10 deg. Period: 664.30 min. COSPAR: 1976-041A. USAF Sat Cat: 8833. Decay Date: 1990-04-14. Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programmes to stations in the Orbita and participating international networks (international cooperation scheme). References: 2, 6.
1976 May 13 - 22:28 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36A. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3D Centaur. LV Configuration: SLV-3D Centaur AC-38 / Centaur D-1AR 5020.
  • Comstar 1 Nation: USA. Program: Comstar. Payload: Comstar 1A. Mass: 792 kg (1,746 lb). Class: Communications. Spacecraft: Intelsat 4A. Agency: Comsat. Perigee: 35,903 km (22,309 mi). Apogee: 35,925 km (22,322 mi). Inclination: 12.70 deg. Period: 1,442.60 min. COSPAR: 1976-042A. USAF Sat Cat: 8838. Completed Operations Date: 1984-10-26. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit over the Americas at 128 deg W in 1976-1981 over the Americas at 95 deg W in 1981-1983 over the Atlantic Ocean 76 deg W in 1983-1984 As of 4 September 2001 located at 48.64 deg E drifting at 1.641 deg W per day. As of 2007 Mar 10 located at 31.21E drifting at 1.624W degrees per day. References: 2, 6, 278.
1976 May 15 - 13:30 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Meteor 1-25 Nation: USSR. Payload: Meteor-Priroda s/n 2-1. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor-Priroda. Agency: MOM. Perigee: 829 km (515 mi). Apogee: 884 km (549 mi). Inclination: 81.30 deg. Period: 102.10 min. COSPAR: 1976-043A. USAF Sat Cat: 8845. Continuation of experimental work in studying the natural resources of the earth. References: 2, 6.
1976 May 17 - Launch Site: Baikonur. Launch Complex: LC177. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • State trials flight Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1976 May 17 - Launch Site: Baikonur. Launch Complex: LC105. Launch Pad: -. Launch Vehicle: R-36M.
  • SLI? Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1976 May 17 - 16:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.33NP.
  • SPAR 2 Microgravity mission Nation: USA. Agency: NASA. Apogee: 188 km (116 mi). References: 2.
1976 May 18 - 11:00 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 818 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 78. Mass: 400 kg (880 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 271 km (168 mi). Apogee: 481 km (298 mi). Inclination: 71.10 deg. Period: 92.10 min. COSPAR: 1976-044A. USAF Sat Cat: 8851. Completed Operations Date: 1977-01-05. Decay Date: 1977-03-07. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1976 May 18 - 17:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 GL A03.410-1.
  • Solar XUV / UV Solar ultraviolet and x-ray mission Nation: USA. Agency: USAF GL. Apogee: 190 km (110 mi). References: 2.
1976 May 20 - 09:00 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 819 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 207 km (128 mi). Apogee: 293 km (182 mi). Inclination: 64.90 deg. Period: 89.50 min. COSPAR: 1976-045A. USAF Sat Cat: 8853. Duration: 11.00 days. Decay Date: 1976-06-01. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1976 May 21 - 07:00 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 820 Nation: USSR. Program: Resurs. Payload: Zenit-4MKT no. 2. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MKT. Agency: MOM. Perigee: 209 km (129 mi). Apogee: 217 km (134 mi). Inclination: 81.40 deg. Period: 88.80 min. COSPAR: 1976-046A. USAF Sat Cat: 8856. Duration: 12.00 days. Decay Date: 1976-06-02. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. References: 2, 6, 103.
1976 May 22 - 07:42 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B-1. LV Configuration: Scout B-1 S179CR.
  • P 76-5 Nation: USA. Mass: 73 kg (160 lb). Class: Technology. Type: Comsat. Spacecraft: P 76. Agency: USAF STP. Perigee: 981 km (609 mi). Apogee: 1,044 km (648 mi). Inclination: 99.60 deg. Period: 105.40 min. COSPAR: 1976-047A. USAF Sat Cat: 8860. Communications propagation experiments. References: 2, 6.
1976 May 23 - 09:30 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.48NP.
  • SFHe Experiment Technology mission Nation: USA. Agency: NASA. Apogee: 196 km (121 mi). References: 2.
1976 May 24 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100N. FAILURE: Failure.
  • Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1976 May 25 - 22:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 May 26 - 09:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 821 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 314 km (195 mi). Inclination: 72.80 deg. Period: 89.70 min. COSPAR: 1976-048A. USAF Sat Cat: 8862. Duration: 13.00 days. Decay Date: 1976-06-08. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1976 May 27 - 00:30 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7. LV Configuration: Skylark 7 SL1211.
  • Test / ionosphere mission Nation: UK. Agency: BAC. Apogee: 254 km (157 mi). References: 2.
1976 May 28 - 15:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53716-328.
  • Cosmos 822 Nation: USSR. Mass: 550 kg (1,210 lb). Class: Calibration. Spacecraft: Taifun-1. Agency: MO SSSR. Perigee: 280 km (170 mi). Apogee: 711 km (441 mi). Inclination: 74.10 deg. Period: 94.50 min. COSPAR: 1976-049A. USAF Sat Cat: 8865. Decay Date: 1978-08-08. Radar calibration mission. References: 2, 6.
1976 May 29 - 09:49 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sandhawk. Model: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia.
  • LEINAX IV X-ray astronomy mission Nation: Japan. Agency: Sandia. Apogee: 271 km (168 mi). References: 2.
1976 May 31 -
  • Yantar-1KFT development approved. Nation: USSR. Spacecraft: Yantar-1KFT. Decree 409-147 'On Creation of Yantar-1KFT Space Complex for Solving Goals of Cartography--development of the Yantar-1KFT reconnaissance satellite' was issued. References: 474.
1976 June 1 - Launch Site: Jiuquan. Launch Complex: -. Launch Pad: -. Launch Vehicle: DF-4.
  • Date uncertain. First test of DF-4. Nation: China. Program: Long March. References: 87.
1976 June 1 - Launch Site: Biscarosse. Launch Complex: BLB. Launch Pad: -. Launch Vehicle: SSBS. Model: SSBS S2. LV Configuration: SSBS S2 S-1E-2606.
  • Operational test Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi). References: 2.
1976 June 2 - 20:56 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 34B. LV Configuration: Titan 34B 34B-5 (3B-55) / Ascent Agena D.
  • SDS no. 1 Nation: USA. Payload: SDS no. 1. Mass: 700 kg (1,540 lb). Class: Communications. Type: Military. Spacecraft: SDS. Agency: NRO/USAF. Perigee: 380 km (230 mi). Apogee: 39,315 km (24,429 mi). Inclination: 63.30 deg. Period: 703.80 min. COSPAR: 1976-050A. USAF Sat Cat: 8871. References: 2, 6.
1976 June 2 - 22:30 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-283.
  • Cosmos 823 Nation: USSR. Mass: 650 kg (1,430 lb). Class: Navigation. Spacecraft: Tsiklon. Agency: MO SSSR. Perigee: 971 km (603 mi). Apogee: 1,007 km (625 mi). Inclination: 83.00 deg. Period: 104.90 min. COSPAR: 1976-051A. USAF Sat Cat: 8873. Military navigation satellite. References: 2, 6.
1976 June 4 - 04:23 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P187H.
  • E field / VLF Ionosphere mission Nation: UK. Agency: SRC. Apogee: 143 km (88 mi). References: 2.
1976 June 4 - 04:39 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P144H.
  • VLF Ionosphere mission Nation: UK. Agency: SRC. Apogee: 132 km (82 mi). References: 2.
1976 June 6 - 08:44 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sandhawk. Model: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia.
  • X-ray astronomy mission Nation: USA. Agency: Sandia. Apogee: 430 km (260 mi). References: 2.
1976 June 8 - 07:00 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 824 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 325 km (201 mi). Inclination: 71.40 deg. Period: 89.80 min. COSPAR: 1976-052A. USAF Sat Cat: 8877. Duration: 13.00 days. Decay Date: 1976-06-21. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1976 June 9 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • FOT GT127M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1976 June 9 - Launch Site: Baikonur. Launch Complex: LC106. Launch Pad: -. Launch Vehicle: R-36M.
  • Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1976 June 10 - 00:09 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2914. LV Configuration: Delta 2914 601/D124.
  • Marisat 2 Nation: USA. Payload: Marisat 102. Mass: 362 kg (798 lb). Class: Communications. Spacecraft: Marisat. Agency: Comsat. Perigee: 36,513 km (22,688 mi). Apogee: 37,604 km (23,365 mi). Inclination: 14.90 deg. Period: 1,501.60 min. COSPAR: 1976-053A. USAF Sat Cat: 8882. Completed Operations Date: 1996-09-25. Maritime communications. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Pacific Ocean at 176 deg E in 1976-1991 over the Pacific Ocean 178 deg W in 1991-1996 As of 5 September 2001 located at 158.48 deg W drifting at 15.761 deg W per day. As of 2007 Mar 10 located at 162.62W drifting at 15.745W degrees per day. References: 2, 6.
1976 June 10 - 17:40 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7 AC. LV Configuration: Skylark 7 AC SL1212.
  • XRCS X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 280 km (170 mi). References: 2.
1976 June 11 - Launch Vehicle: Energia.
  • Buran design selected. Nation: USSR. Spacecraft: Buran. Decree 'On selection of design layout for Buran' was issued. Following exhaustive analysis and inability to improve on the design, a straight aerodynamic copy of the US space shuttle, was selected as the Buran orbiter configuration. MiG was selected as subcontractor to build the orbiter. For this purpose MiG spun off a new design bureau, Molniya, with G E Lozino-Lozinskiy as chief designer. References: 474.
1976 June 11 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. Model: Nike Javelin. LV Configuration: Nike Javelin NASA 32.04WT.
  • Test mission Nation: USA. Agency: NASA. Apogee: 130 km (80 mi). References: 2.
1976 June 14 -
  • Start aft fuselage assembly (STA-099) Nation: USA. Program: STS. References: 15.
1976 June 15 - Launch Vehicle: Energia.
  • Decree authorising development of 11B97 nuclear electric rocket stage Nation: USSR. Spacecraft: Mars 1986. Decree 'On course of work on nuclear rocket engines' was issued. The 11B97 stage would have an electric capacity of 500-600 kW and would use specialised plasma-ion electric engines using standing plasma waves and anodes. It was powered from a reactor with a 200 litre core containing 30 kg of uranium fuel. In 1978 this engine was studied for use as a reusable interorbital space tug for launch by Energia-Buran. References: 474.
1976 June 15 - Launch Site: Baikonur. Launch Complex: LC170. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1976 June 15 - 13:19 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-277.
  • Cosmos 825 Nation: USSR. Program: Strela. Payload: Strela-1M no. 113. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,395 km (866 mi). Apogee: 1,487 km (923 mi). Inclination: 74.00 deg. Period: 114.70 min. COSPAR: 1976-054A. USAF Sat Cat: 8889. Eight satellites launched by a single carrier rocket. References: 2, 6.
  • Cosmos 826 Nation: USSR. Program: Strela. Payload: Strela-1M no. 114. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,482 km (920 mi). Apogee: 1,545 km (960 mi). Inclination: 74.00 deg. Period: 116.30 min. COSPAR: 1976-054B. USAF Sat Cat: 8890. References: 2, 6.
  • Cosmos 827 Nation: USSR. Program: Strela. Payload: Strela-1M no. 115. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,413 km (877 mi). Apogee: 1,489 km (925 mi). Inclination: 74.00 deg. Period: 114.90 min. COSPAR: 1976-054C. USAF Sat Cat: 8891. References: 2, 6.
  • Cosmos 828 Nation: USSR. Program: Strela. Payload: Strela-1M no. 116. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,432 km (889 mi). Apogee: 1,489 km (925 mi). Inclination: 74.00 deg. Period: 115.10 min. COSPAR: 1976-054D. USAF Sat Cat: 8892. References: 2, 6.
  • Cosmos 829 Nation: USSR. Program: Strela. Payload: Strela-1M no. 117. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,451 km (901 mi). Apogee: 1,490 km (920 mi). Inclination: 74.00 deg. Period: 115.30 min. COSPAR: 1976-054E. USAF Sat Cat: 8893. References: 2, 6.
  • Cosmos 830 Nation: USSR. Program: Strela. Payload: Strela-1M no. 118. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,469 km (912 mi). Apogee: 1,493 km (927 mi). Inclination: 74.00 deg. Period: 115.60 min. COSPAR: 1976-054F. USAF Sat Cat: 8894. References: 2, 6.
  • Cosmos 831 Nation: USSR. Program: Strela. Payload: Strela-1M no. 119. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,475 km (916 mi). Apogee: 1,507 km (936 mi). Inclination: 74.00 deg. Period: 115.80 min. COSPAR: 1976-054G. USAF Sat Cat: 8895. References: 2, 6.
  • Cosmos 832 Nation: USSR. Program: Strela. Payload: Strela-1M no. 120. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,482 km (920 mi). Apogee: 1,521 km (945 mi). Inclination: 74.00 deg. Period: 116.00 min. COSPAR: 1976-054H. USAF Sat Cat: 8896. References: 2, 6.
1976 June 16 - 13:10 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 833 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 180 km (110 mi). Apogee: 316 km (196 mi). Inclination: 62.80 deg. Period: 89.40 min. COSPAR: 1976-055A. USAF Sat Cat: 8898. Duration: 13.00 days. Decay Date: 1976-06-29. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1976 June 17 - 05:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.17UH.
  • SAO XR X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 232 km (144 mi). References: 2.
1976 June 17 - 07:47 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7 AC. LV Configuration: Skylark 7 AC SL1501.
  • Coded mask telescope X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 256 km (159 mi). References: 2.
1976 June 18 - 11:41 GMT - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1 S193C.
  • GP-A Physics mission Nation: USA. Agency: NASA. Apogee: 10,230 km (6,350 mi). References: 2.
1976 June 19 - 16:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-276.
  • Intercosmos 15 Nation: USSR. Program: Intercosmos. Payload: AUOS-Z-T-IK. Mass: 550 kg (1,210 lb). Class: Technology. Spacecraft: AUOS. Manufacturer: NPO Yuzhnoye. Agency: IK. Perigee: 481 km (298 mi). Apogee: 520 km (320 mi). Inclination: 74.00 deg. Period: 94.60 min. COSPAR: 1976-056A. USAF Sat Cat: 8903. Completed Operations Date: 1976-07-26. Decay Date: 1979-11-18. Testing of new systems and components of satellite under space flight conditions. References: 2, 6, 116.
1976 June 21 - 07:01 GMT - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • OT GT33GM operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1976 June 22 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • FOT GT128M Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.
1976 June 22 - 18:04 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K. LV Configuration: Proton-K 290-02.
  • Salyut 5 Nation: USSR. Program: Almaz. Payload: Almaz s/n 103-01. Mass: 19,000 kg (41,000 lb). Class: Manned. Type: Space station. Spacecraft: Almaz OPS. Agency: MOM. Perigee: 215 km (133 mi). Apogee: 232 km (144 mi). Inclination: 51.60 deg. Period: 88.90 min. COSPAR: 1976-057A. USAF Sat Cat: 8911. Duration: 411.24 days. Decay Date: 1977-08-08. Second successful flight of the Almaz manned military space station. It had taken only 60 days and 1450 man-hours to prepare Almaz 0101-2 for flight, using the services of 368 officers and 337 non-commissioned officers. The tracking ships Academician Sergei Korolev and Cosmonaut Yuri Gagarin were stationed in the Atlantic and Caribean to provide communications when out of tracking range of the USSR. Salyut 5 operated for 409 days, during which the crews of Soyuz 22 and 24 visited the station. Soyuz 23 was to have docked but its long-distance rendezvous system failed. Soyuz 25 was planned, but the mission would have been incomplete due to low orientation fuel on Salyut 5, so it was cancelled.

    During the flight of Salyut 5 a 'parallel crew' was aboard a duplicate station on the ground. They conducted the same operations in support of over 300 astrophysical, geophysical, technological, and medical/biological experiments. Astrophysics studies included an infrared telescope-spectrometer in the 2-15 micrometer range which also obtained solar spectra. Earth resources studies were conducted as well as Kristall, Potok, Diffuziya, Sfera, and Reatsiya technology experiments. Presumably Salyut 5 was equipped with a SAR side-looking radar for reconnaissance of land and sea targets even through cloud cover.

    The film capsule was ejected 22 February 1977 (and sold at Sotheby's, New York, on December 11, 1993!). The station was deorbited on 8 August 1977. In addition to the human crew two Russian tortoises (Testudo horsfieldi) and Zebrafish (Danio rerio) were flown.

    The results of the Salyut 3 and 5 flights showed that manned reconnaissance was not worth the expense. There was minimal time to operate the equipment after the crew took the necessary time for maintenance of station housekeeping and environmental control systems. The experiments themselves showed good results and especially the value of reconnaissance of the same location in many different spectral bands and parts of the electromagnetic spectrum. Additional Details: Salyut 5. References: 2, 6, 67, 274.

1976 June 22 - 20:16 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-20? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 June 22 - 20:17 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-20? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 June 24 -
  • Complete MPTA-098 proof load test Nation: USA. Program: STS. Complete MPTA-098 proof load test, Lockheed test site and on dock, Palmdale References: 15.
1976 June 24 - 07:10 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 834 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 216 km (134 mi). Apogee: 237 km (147 mi). Inclination: 81.40 deg. Period: 89.10 min. COSPAR: 1976-058A. USAF Sat Cat: 8914. Duration: 12.00 days. Decay Date: 1976-07-06. Area survey photo reconnaissance satellite; returned film capsule. References: 2, 6.
1976 June 24 - 23:40 GMT - Launch Site: Syowa Base. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210JA-20.
  • VLF / HF / ne Aurora mission Nation: Japan. Agency: NIPR. Apogee: 118 km (73 mi). References: 2.
1976 June 25 -
  • Complete functional checkout, Enterprise (OV-101) Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise. References: 15.
1976 June 26 - Launch Site: Baikonur. Launch Complex: LC173. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1976 June 26 - 03:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC40. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. LV Configuration: Titan IIIC 23C-10 (3C-28).
  • IMEWS 6 Nation: USA. Payload: DSP Phase 2 s/n 8. Mass: 1,040 kg (2,290 lb). Class: Early Warning. Spacecraft: DSP. Agency: USAF. Perigee: 35,620 km (22,130 mi). Apogee: 35,860 km (22,280 mi). Inclination: 0.50 deg. Period: 1,433.30 min. COSPAR: 1976-059A. USAF Sat Cat: 8916. Completed Operations Date: 1984-07-01. Second generation geosynchronous ballistic missile launch detection satellite, remained in service for over eight years. Positioned over the Atlantic Ocean from 1976 to 1981: at 35 deg W in 1976-1977; at 65 deg W in 1977-1979; and 35 deg W in 1979-1980; and 65 deg W in 1980-1981. Then moved over the Pacific Ocean at 125 deg W, then 140 deg W in 1981-1982; then over the Indian Ocean at 75 deg E in 1982-1984. References: 2, 6, 127.
1976 June 26 - 08:58 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-21? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 June 26 - 09:06 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-21? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1976 June 27 - Launch Site: Kwajalein. Launch Complex: RN. Launch Pad: -. Launch Vehicle: Sergeant. Model: Castor. LV Configuration: Castor-2R.
  • Technology mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1976 June 27 - 08:58 GMT - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 4B. LV Configuration: Black Brant IVB Astro 6-2.
  • DLR H-BB4B-76 Extreme ultraviolet astronomy mission Nation: Germany. Agency: DLR. Apogee: 700 km (430 mi). References: 2.
1976 June 28 -
  • Start horizontal ground vibration tests Enterprise Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise. Start horizontal ground vibration tests and proof load tests, Enterprise (OV-101) References: 15.
1976 June 28 - 02:40 GMT - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-17.
  • ITF-1 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). Last launch of a Titan II ICBM (first West Coast launch on 16 February 1963). Demonstrated new Universal Space Guidance System for launch vehicle variant. References: 2.
1976 June 29 - Launch Site: Baikonur. Launch Complex: LC177. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1976 June 29 - Launch Site: Baikonur. Launch Complex: LC103. Launch Pad: -. Launch Vehicle: R-36M.
  • Missile accuracy test launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). References: 2.
1976 June 29 - 07:20 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 835 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 174 km (108 mi). Apogee: 317 km (196 mi). Inclination: 65.00 deg. Period: 89.40 min. COSPAR: 1976-060A. USAF Sat Cat: 8922. Duration: 13.00 days. Decay Date: 1976-07-12. High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 2, 6.
1976 June 29 - 08:12 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-284.
  • Cosmos 836 Nation: USSR. Program: Strela. Mass: 750 kg (1,650 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 773 km (480 mi). Apogee: 801 km (497 mi). Inclination: 74.10 deg. Period: 100.60 min. COSPAR: 1976-061A. USAF Sat Cat: 8923. References: 2, 6.
1976 June 29 - 18:20 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.181GA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi). References: 2.
1976 June 29 - 18:20 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.130GS.
  • Solar Constant 1 Solar mission Nation: USA. Agency: NASA. Apogee: 225 km (139 mi). References: 2.
1976 June 30 -
  • SSME dummy set on dock, Palmdale. Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise. SSME dummy set on dock, Palmdale, Enterprise (OV-101) References: 15.
1976 June 30 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Kookaburra.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 120 km (70 mi). References: 2.
1976 June 30 - 09:19 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 3.
  • FOT GT54GM Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). References: 2.

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