Army Jupiter IRBM was fired 1,500 miles, limit of its designed range, and to an altitude of 250-300 miles, the first successful launching of an IRBM. Fired from AMR at 1308 hours EST to test the range capability and performance of rocket engine and control system. Although the missile was 253 nm short of its estimated 1,400 nm impact point, this was the first successful flight of the Jupiter. All phases of the test were successful during this first firing of the IRBM in the western world
Washington discussion of the Air Force Man-In-Space proposal continued to ferment without any sign of the approval necessary to start the program. The Advanced Research Projects Agency indicated general agreement with the Air Force space development plan and the National Security Council Planning Board displayed a "feeling of great urgency to achieve animal flights in space with safe return and to achieve the Man-In-SpaceSoonest at the earliest possible date." Other than this nebulous progress the Air Force man in space effort was no nearer realization. (Memo, Col H. L. Evans, Asst Dep Cmdr, Space Sys, to Col C. H. Terhune, 31 May 58, subj: Trip Report.)
STG submitted to NASA Headquarters recommendations on crew selection and training:
Second launch of a quadruplet of Poppy naval signals intelligence satellites, which would lead to the NOSS production series. Official and secondary mission: Gravity gradient stabilization tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Soyuz 9 State Commission meets at Area 31 at 11:00. That evening the spacecraft will be integrated with the booster, with roll-out to the pad scheduled for the following morning at 05:00. At 17:00 the cosmonauts give a formal interview to the Russian 'Parade' magazine. After that they hold a general press conference.
Kamanin is advised that the atmosphere aboard Salyut 1 is now all right. He finds the news disturbing, since he was not informed until then that there was a problem! Feoktistov outlines the modifications made to Soyuz 11 compared to Soyuz 10 to the cosmonauts. The reinforcement of the docking ring system has added 10 kg to the spacecraft. Consumables are carried that increase the time for autonomous flight from three to four days.
Mir module; materials processing laboratory. Docked with Mir. Kristall: Mass: 19,500 kg. Mass on docking 17,200 kg. Length: 11. 9 m or 13. 73 m?. Solar array span 36 m. Diameter: 4. 35 m. Payload: 7,000 kg. Two compartments. Instrument-Payload Compartment contains food containers, and industrial processing units Krater 3, Optizon 1, Zona 02, and Zona 03. 0. 8 m hatch leads to Junction-Docking compartment. This contains spherical universal docker with two APAS-89 androgynous docking units. These will be used to dock with Buran shuttle and 1,000 kg X-ray telescope to be delivered by Buran in 1991. Third opening houses earth observation cameras.
Launch originally planned for 30 March 1990. Delayed to April 18, then further delayed due to computer chip problems.
Launched 31 May 1990 12:33 GMT. Docking scheduled June 6 at 12:36 but delayed due to problem with one of Kristall's orientation engines. Docking successful 10 June at 12:47. On June 11 moved to side port. Work within module began 15 June.
Spektr: Late 1991 launch. Remote sensing work. Occupies port opposite Kvant 2. Before this occurs Kristall solar arrays will be relocated to Kvant.
Officially: Specialized module. Experimental-industrial production of semi-conducting materials; refinement of biologically active substances for the production of new medicinal preparations. Cultivation of crystals of different albumine compositions and hybridizatio n of cells. Conduct of astrophysical and technical experiments.
This EVA started on 30.05 at 1820 UTC (opening of the hatch) and ended on 30.05. at 2240 UTC (closing of the hatch). The MOMS-2 camera (Modular Opto-electronic Multi-spectral/ Stereo scanner has been installed on the outer surface of the module Priroda. The 2d task was the installation of an extra handrail outside Priroda to facilitate EVA's. The EVA passed without problems.
Microgravity mission with the experiments being returned to earth after 16 days in a spherical Vostok capsule of the type that first carried Yuri Gagarin into space in 1961. The capsule landed in Kazakhstan at 07:36 GMT on 16 June. For this mission a 385 kg European payload of 39 experiments in fluid physics, biology, material science, meteoritics, radiation dosimetry and exobiology was carried. A further 215 kg of Russian instruments were also flown. Many were experiments were being reflown following loss of Foton-M1 on 15 October 2002. The planned Fotino miniature re-entry capsule experiment was not flown.
Applied research included heat transfer experiments with the European FluidPac facility, chemical diffusion experiments in the SCCO (Soret Coefficients in Crude Oil), and material science investigations in the Agat and Polizon furnaces. These experiments were expected to contribute to new heat-exchanger designs, more efficient oil exploration processes, and better semiconductor alloys. The Biopan facility carried life science experiments, including a student seed germination test.
Discovery delivered to the International Space Station the Kibo Pressurized Module, the primary element of the Japanese portion of the station. Half an earth away from jettison of external tank ET-128, a 76 m/s OMS-2 burn at 21:40 GMT put the Shuttle in its low-altitude chase lorbit. Discovery docked at the PMA-2 port of the station at 18:03 GMT on 2 June. Using the shuttle and station's robotic arms, with assistance from spacewalking astronauts, the Kibo module was attached to the station's Harmony module at 23:01 GMT on 4 June. The previously-delivered Japanese Logistics Module was transferred from Harmony to Kibo on 6 June at 20:04 GMT. The Shuttle undocked from the station on 11 June at GMT and landed on 14 June at 15:15 GMT at the Kennedy Space Center.