Encyclopedia Astronautica
January 08


January 08 Chronology


1898 January 8 - .
  • Birth of Ludwig Leihfeld - . Nation: Germany; Russia. Summary: German engineer in WW2, member of the Rocket Team in the Soviet Union, worked on rocket engine development in Glushko's design bureau from 1947 to 1952. Worked in Oxygen Plant; Dept. 61/ Laboratory..

1900 January 8 - .
1909 January 8 - .
  • Birth of Friedrich Wilhelm Schwarz - . Nation: Germany; USA. Summary: German-American engineer in WW2, member of the Rocket Team in the United States thereafter. German expert in guided missiles during WW2. As of January 1947, working at Fort Bliss, Texas. Died at Phoenix, Arizona..

1910 January 8 - .
  • Birth of Heinz Haase - . Nation: Germany; Russia. Summary: German engineer in WW2, member of the Rocket Team in the Soviet Union thereafter. Graduate engineer who worked on rocket engine development in Glushko's design bureau from 1947 to 1952. Worked as Deputy in charge of the Oxygen Plant..

1922 January 8 - .
  • Birth of Dale Dehaven Myers - . Nation: USA. Summary: American aerodynamicist, charismatic manager that went many times through the revolving door between industry and government. Key roles in Hound Dog, Apollo, Shuttle, and B-1 programs..

1942 January 8 - .
1943 January 8 - . LV Family: V-2. Launch Vehicle: V-2.
  • Showdown meeting on A4 - . Nation: Germany. Related Persons: Degenkolb; Dornberger; Hitler; Speer; Todt. Speer meets with Von Braun and Dornberger. A 1:100 model of the planned bunker construction-launch facility for the rocket to be built by Organisation Todt on the British channel was exhibited. Speer reveals that Hitler could not decide about the rocket as a weapon. He did not believe the rocket team's plans could be made to work. But Speer did authorise them to proceed with construction on his own authority - he hoped Hitler could be brought around eventually. But he emphasised that Dornberger would have to use his personal connections to get industry moving on the project. But Dornberger was thwarted when the Army put Degenkolb in charge of organising production of the missile. Degenkolb was a sworn enemy of Dornberger's, and had been implicated in the 'suicide' of General Becker in early 1940. Degenkolb set up a Nazi-supported bureaucracy in parallel to that of Dornberger's, requiring the approval of the Army weapons bureau on any decisions. Degenkolb had the sponsorship of Todt and Saur, who in turn followed the party line - 'like the Fuehrer, we are not yet won over to the concept of a long range missile'.

    In order to productionise the A4 design, Degenkolb began authorising many detailed changes. He didn't understand that every change had to be proven in test first, and only incremental steps could be taken. Stahlknecht had planned to produce 300 A4 missiles per month by January 1944, and 600 per month by July 1944. Degenkolb unrealistically decreed that 300 per month be achieved by October 1943, and 900 per month by December 1943.


1943 January 8 - . Launch Vehicle: JATO.
  • First JATO takeoff. - . Nation: USA. Summary: First aircraft takeoff in United States with permanently installed JATO rocket powerplant, an A-20A at Muroc Army Air Base, Calif..

1944 January 8 - . Launch Site: Heidelager. LV Family: V-2. Launch Vehicle: V-2. FAILURE: Failure.
1945 January 8 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 20843. FAILURE: Air-burst of rocket but explosion of warhead at ground level..
  • V-2 Ma419 326 X19 - . Nation: Germany. Agency: Wehrmacht. Summary: Planned range 225 km. Air-burst of rocket but explosion of warhead at ground level 1.8 km to the left of the planned trajectory. Circular error 6.3 km from aim point..

1947 January 8 - .
  • XS-1 Flight 17 - . Crew: Goodlin. Payload: XS-1 # 2 flight 7. Nation: USA. Related Persons: Goodlin. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: Bell flight 7. Buffet boundary investigation. Mach 0.80 at 10675 m..

1948 January 8 - .
  • XS-1 Flight 62 - . Crew: Hoover. Payload: XS-1 # 2 flight 24. Nation: USA. Related Persons: Hoover. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: NACA flight 4. Turns and pull-ups to buffet. Mach 0.83..

1951 January 8 - .
  • Birth of Taufik Akbar - . Nation: Indonesia. Summary: Indonesian engineer payload specialist astronaut, 1985-1986..

1953 January 8 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 158R.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1954 January 8 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador GM-11109.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1957 January 8 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17. LV Configuration: X-17 R-18 4203-18.
  • Re-entry vehicle test - . Nation: USA. Agency: USAF. Apogee: 140 km (80 mi).

1958 January 8 - . Launch Site: White Sands. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp II8.35.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 145 km (90 mi).

1959 January 8 - . LV Family: Redstone. Launch Vehicle: Redstone MRLV.
  • Redstones ordered for Mercury suborbital launches. - . Nation: USA. Related Persons: von Braun. Program: Mercury. Summary: NASA requested eight Redstone-type launch vehicles from the Army to be used in Project Mercury development flights..

1960 January 8 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1X-7.
  • Inertial test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1962 January 8 - .
  • Dyna-Soar Step III study halted. - . Nation: USA. Spacecraft: Dynasoar. Summary: AFSC headquarters halted any further consideration of a Step III study..

1963 January 8 - .
  • Existing C-band tracking radars to be modified to increase range for Apollo - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Communications. After studying the present radar coverage provided by ground stations for representative Apollo trajectories, North American recommended that existing C-band radars be modified to increase ranging limits. The current capability for tracking to 920 kilometers (500 nautical miles), while satisfactory for near-earth trajectories, was wholly inadequate for later Apollo missions. Tracking capability should be extended to 59,000 kilometers (32,000 nautical miles), North American said; and to improve tracking accuracy, transmitter power and receiver sensitivity should be increased.

1964 January 8 - .
  • NASA criticises Manned Orbiting Laboratory. - . Nation: USA. Spacecraft: MORL. In an interview for Space Business Daily, Edward Z. Gray, Director of Advanced Studies in NASA's Office of Manned Space Flight, predicted that NASA's manned space station would be more sophisticated than the Defense Department's Manned Orbiting Laboratory. NASA had more than a dozen study projects under way, Gray said, that when completed would enable the agency to appraise requirements and pursue the best approach to developing such a space station.

1964 January 8 - . 00:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3X-50.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1964 January 8 - . 13:15 GMT - . Launch Site: Thumba. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.129IA.
  • ISRO 10.02? (Na) Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 187 km (116 mi).

1964 January 8 - . 20:10 GMT - . Launch Site: Mud Lake DZ. Launch Pad: 37.9 N x 117.1 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-43-69. FAILURE: Inertial instruments failure..
  • X-15A SAS Off Stability test - . Nation: USA. Agency: NASA; USAF. Apogee: 42 km (26 mi). Summary: Maximum Speed - 5818 kph. Maximum Altitude - 42642 m..

1965 January 8 - . 18:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 106F.
  • ST - . Nation: USA. Agency: USAF SAC. Apogee: 1,400 km (800 mi).

1966 January 8 - .
  • Space trainers - . Nation: USSR. Related Persons: Tyulin; Mozzhorin; Korolev. Program: Voskhod; Soyuz. Flight: Voskhod 3; Voskhod 4; Voskhod 5; Soyuz 1; Soyuz 2A. Spacecraft: Voskhod; Soyuz 7K-OK. Tyulin and Mozzhorin review space simulators at TsPK. The 3KV and Volga trainers are examined. Tyulin believes the simulators need to be finished much earlier, to be used not just to train cosmonauts, but as tools for the spacecraft engineers to work together with the cosmonauts in establishing the cabin arrangement. This was already done on the 3KV trainer, to establish the new, more rational Voskhod cockpit layout. Tyulin reveals that the female Voskhod flight now has the support of the Central Committee and Soviet Ministers. He also reveals that MOM has promised to accelerate things so that four Voskhod and five Soyuz flights will be conducted in 1966. For 1967, 14 manned flights are planned, followed by 21 in 1968, 14 in 1969, and 20 in 1970. This adds up to 80 spaceflights, each with a crew of 2 to 3 aboard. Tyulin also supports the Kamanin position on other issues - the Voskhod ECS should be tested at the VVS' IAKM or Voronin's factory, not the IMBP. The artificial gravity experiment should be removed from Voskhod and replaced by military experiments. He promises to take up these matters with Korolev.

1966 January 8 - . 04:48 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC10W. LV Family: Delta. Launch Vehicle: Thor Burner 1. LV Configuration: Thor Burner 1 251. FAILURE: Second stage failed.. Failed Stage: 2.
  • DMSP-Block-4A F5 - . Payload: DAPP 14/OPS 2394. Mass: 130 kg (280 lb). Nation: USA. Agency: USAF. Program: DMSP. Class: Earth. Type: Weather satellite. Spacecraft: DMSP Block 4A. Decay Date: 1966-01-06 . COSPAR: F660108A. Summary: Defense Meteorological Satellite Program..

1966 January 8 - . 13:11 GMT - . Launch Site: Thumba. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C103 TERLS-35.
  • ISRO 15.03 Aeronomy / ionosphere mission - . Nation: India. Agency: ISRO. Apogee: 150 km (90 mi).

1967 January 8 - . 10:02 GMT - . Launch Site: Sea-launched. Launch Pad: M9185. Launch Platform: SHIP-SOV. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Agency: GMS. Apogee: 80 km (49 mi).

1968 January 8 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 608. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2P-273.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1969 January 8 - .
  • Concern over the possibility of Soyuz 4 or 5 landing in the Aral Sea continues. - . Nation: USSR. Program: Soyuz. Flight: Soyuz 4; Soyuz 5; Soyuz 4/5. Spacecraft: Soyuz 7K-OK. An Il-14 is sent on a flight to reconnoitre. It reports 12 to 50 cm ice over the entire surface. Mishin, Chertok, and the rest of he OKB-1 entourage arrive. An argument immediately ensures over provisions and planning for emergency landings. It is decided to make a review of emergency landing and recovery plans as the first agenda item every day of he flights.

1969 January 8 - .
1969 January 8 - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: S-250. LV Configuration: S-250 SO-250-B.
  • Test mission - . Nation: Japan. Agency: ISAS. Apogee: 100 km (60 mi).

1969 January 8 - . 02:10 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-25.
  • Gyro-plasma probe Ionosphere / chemical release / fields mission - . Nation: Japan. Agency: ISAS. Apogee: 343 km (213 mi).

1970 January 8 - .
  • Dale D. Myers was appointed NASA Associate Administrator for Manned Space Flight. - . Nation: USA. Related Persons: Mueller. Dale D. Myers was appointed NASA Associate Administrator for Manned Space Flight with an effective date of 12 January. He succeeded George E. Mueller, who left NASA on 10 December 1969 to become a vice president of General Dynamics Corporation. Prior to his acceptance of the NASA position, Myers was Vice President and General Manager of the Space Shuttle Program at North American Rockwell.

1971 January 8 - . 21:41 GMT - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.016-3.
  • Sphere Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 278 km (172 mi).

1971 January 8 - . 22:11 GMT - . Launch Site: Green River. Launch Complex: Green River Pad 3. LV Family: Athena RTV. Launch Vehicle: Athena RTV. LV Configuration: Athena V144D.
  • Re-entry Vehicle test - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1971 January 8 - . 22:31 GMT - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.015-2.
  • Sphere Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 276 km (171 mi).

1972 January 8 - . 09:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1973 January 8 - . 06:55 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K/D. LV Configuration: Proton-K/D 259-01.
  • Luna 21 - . Payload: Ye-8 s/n 204. Mass: 5,567 kg (12,273 lb). Nation: USSR. Agency: MOM. Program: Luna. Class: Moon. Type: Lunar probe. Spacecraft: Luna Ye-8. Decay Date: 1973-01-15 . USAF Sat Cat: 6333 . COSPAR: 1973-001A. Apogee: 110 km (60 mi). Perigee: 90 km (55 mi). Inclination: 60.0000 deg. Period: 118.00 min. The Proton / Block D launcher put the spacecraft into Earth parking orbit followed by translunar injection. On 12 January 1973, Luna 21 braked into a 90 x 100 km orbit about the Moon. On 13 and 14 January, the perilune was lowered to 16 km altitude. On 15 January after 40 orbits, the braking rocket was fired at 16 km altitude, and the craft went into free fall. At an altitude of 750 meters the main thrusters began firing, slowing the fall until a height of 22 meters was reached. At this point the main thrusters shut down and the secondary thrusters ignited, slowing the fall until the lander was 1.5 meters above the surface, where the engine was cut off. Landing occurred at 23:35 GMT in LeMonnier crater at 25.85 degrees N, 30.45 degrees E. The lander carried a bas relief of Lenin and the Soviet coat-of-arms. After landing, Lunokhod 2 took TV images of the surrounding area, then rolled down a ramp to the surface at 01:14 GMT on 16 January and took pictures of the Luna 21 lander and landing site. It stopped and charged batteries until 18 January, took more images of the lander and landing site, and then set out over the Moon. The rover would run during the lunar day, stopping occasionally to recharge its batteries via the solar panels. At night the rover would hibernate until the next sunrise, heated by the radioactive source. Lunokhod 2 operated for about 4 months, covered 37 km of terrain including hilly upland areas and rilles, and sent back 86 panoramic images and over 80,000 TV pictures. Many mechanical tests of the surface, laser ranging measurements, and other experiments were completed during this time. On June 4 it was announced that the program was completed, leading to speculation that the vehicle probably failed in mid-May or could not be revived after the lunar night of May-June. The Lunokhod was not left in a position such that the laser retroreflector could be used, indicating that the failure may have happened suddenly.

1974 January 8 - . 01:40 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.22DG-DP.
  • NRL NB12.271 Aeronomy / extreme ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 193 km (119 mi).

1975 January 8 - . 16:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1976 January 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-12.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 January 8 - . 19:03 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.1008UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 138 km (85 mi).

1979 January 8 - . 16:49 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 71 km (44 mi).

1980 January 8 - . 01:14 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 72 km (44 mi).

1981 January 8 - . 20:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 91 km (56 mi).

1982 January 8 - .
  • Estafeta development approved. - . Nation: USSR. Spacecraft: Estafeta. Development of the military nuclear powered communications satellite was approved by the Soviet VPK Military-Industrial Commission. The satellite would have used the 5 kW nuclear reactor originally planned for the Ekran satellite and used secure uninterceptable laser and radio inter-satellite and space-to-ground communications links. Did not reach flight status before the collapse of the Soviet Union.

1983 January 8 - . 20:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: VOKV. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1984 January 8 - . 20:00 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 16 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 118 km (73 mi).

1985 January 8 - . 13:30 GMT - . Launch Site: Antigua. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 66 km (41 mi).

1986 January 8 - . 11:25 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1715 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 14.00 days. Decay Date: 1986-01-22 . USAF Sat Cat: 16447 . COSPAR: 1986-001A. Apogee: 288 km (178 mi). Perigee: 192 km (119 mi). Inclination: 72.8000 deg. Period: 89.30 min. Summary: Military cartographic satellite; returned film capsule..

1987 January 8 - .
  • International Cosmonaut Training Group selected. - . Nation: Bulgaria. Related Persons: Stoyanov. Summary: Training group of backup Bulgarian guest cosmonaut for a propaganda flights to the Mir space station. This was a 'compensation mission', since the first Bulgarian mission never reached the station due to a primary engine failure aboard the Soyuz shuttle..

1988 January 8 - .
  • Death of Frank Pace at Greenwich, Fairfield, CT. - . Nation: USA. Related Persons: Pace. Summary: American manager, Secretary of the Army, 1950-1953, president of General Dynamics 1953-1962. During his tenure General Dynamics acquired Convair and other companies and became a leading defense and space contractor..

1989 January 8 - . 15:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 62 km (38 mi).

1990 January 8 - . 20:23 GMT - .
1991 January 8 - . 00:53 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 D202.
  • NATO 4A - . Payload: NATO 4A. Mass: 1,433 kg (3,159 lb). Nation: NATO. Agency: NATO. Program: NATO. Class: Communications. Type: Military communications satellite. Spacecraft: ECS/OTS. USAF Sat Cat: 21047 . COSPAR: 1991-001A. Apogee: 35,800 km (22,200 mi). Perigee: 35,775 km (22,229 mi). Inclination: 2.6000 deg. Period: 1,436.10 min. NATO communications; 18 deg W. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit at 18 deg W in 1991-1999 As of 5 September 2001 located at 17.81 deg W drifting at 0.007 deg W per day. As of 2007 Mar 10 located at 16.26W drifting at 0.003W degrees per day.

1994 January 8 - .
  • Death of Kenneth P Timmons - . Nation: USA. Related Persons: Timmons. Summary: American engineer. Headed the Skylab Multiple Docking Adapter and External Tank projects..

1994 January 8 - . 10:05 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Soyuz TM-18 - . Call Sign: Derbent (Derbent - Russian city). Crew: Afanasyev; Polyakov; Usachyov. Backup Crew: Arzamazov; Malenchenko; Strekalov. Payload: Soyuz TM 11F732 s/n 67. Mass: 7,150 kg (15,760 lb). Nation: Russia. Related Persons: Afanasyev; Polyakov; Usachyov; Arzamazov; Malenchenko; Strekalov. Agency: MOM. Program: Mir. Class: Manned. Type: Manned spacecraft. Flight: Mir EO-15; Mir EO-14; Mir LD-4. Spacecraft: Soyuz TM. Duration: 182.02 days. Decay Date: 1994-07-09 . USAF Sat Cat: 22957 . COSPAR: 1994-001A. Apogee: 335 km (208 mi). Perigee: 244 km (151 mi). Inclination: 51.6000 deg. Period: 90.10 min. Summary: Mir Expedition EO-15. Docked at the Kvant module on January 10 at 11:15 GMT. Transported to the Mir orbital station of a crew comprising the cosmonauts V M Afanasev, Y V Usachev, and V V Polyakov for the fifteenth main expedition..

1997 January 8 - . Launch Site: Wallops Island. Launch Vehicle: Hyperion. LV Configuration: Hyperion FPDP 3.
1998 January 8 - . 02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi).

1999 January 8 - .
  • Chinese Module on ISS explored - . Nation: China. Program: ISS. It was reported that China and Russia once discussed docking a Chinese module to the Russian section of the International Space Station. Spare docking ports would provide attachment points for Ukrainian and Chinese modules. Such possibilities had been discussed at the highest political levels.

2008 January 8 - .
  • ISS On-Orbit Status 01/08/08 - . Nation: USA. Related Persons: Love; Malenchenko; Tani; Whitson; Williams, Dave. Program: ISS. Flight: ISS EO-16; ISS EO-16-1; STS-122. CDR Whitson and FE-2 Tani started out with the daily reading of SLEEP (Sleep-Wake Actigraphy and Light Exposure during Spaceflight) experiment data accumulated during the night, for logging and filling in questionnaire entries in the SLEEP session file on the HRF-1 laptop for downlink.

    (To monitor the crewmembers' sleep/wake patterns and light exposure, Dan and Peggy wear a special Actiwatch device which measures the light levels encountered by him as well as his patterns of sleep and activity throughout the Expedition. The log entries are done within 15 minutes of final awakening for seven consecutive days, as part of the crew's discretionary 'job jar' task list.)

    Working in the DC1 Docking Compartment, FE-1 Malenchenko, later joined by CDR Whitson, started a three-day maintenance activity on three Russian Orlan-M spacesuits (#25, #26, #27), first initiating discharge of 825M3 Orlan battery pack #1, then scrubbing and degassing the Orlan water loops, followed by the coolant loops in the DC1 and SM PkhO (Service Module Transfer Compartment) BSS Orlan Interface Units. (Functional inspection & checkout of the suits and their spare parts, including bladder leak tests, are scheduled tomorrow & Thursday.) Additional Details: ISS On-Orbit Status 01/08/08.


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