In a meeting with Professor Hettlage, of the Financial and Organisational Ministry of the German Defence Industry, it was proposed that Peenemuende be made a private country, with the Nazi Party and selected corporations (AEG, Siemens, Lorenz, Rheinmetall) being its shareholders. Dornberger saw Degenkolb behind this plan, and was determined to keep Peenemuende an Army proving ground. He felt that an asset, on which several hundred million Marks had been invested by the government, was being handed over to private hands for 1 to 2 million Marks. The investors intended to recover their entire investment back on a fee paid for each missile built. In the end Dornberger managed to keep Peenemuende an Army proving ground, but then he had to fight off an attempt by AEG to take over the electronics side of the development team. The rocket team's electronic engineers were years ahead of the rest of the industry, and a tempting target.

Council of Soviet Ministers (SM) Decree 'On creation of the submerged submarine-launched ballistic missile' was issued.

Soviet Premier Nikolai A. Bulganin in a letter to President Eisenhower stated that the Soviet Union "is ready to examine also the question of the intercontinental rockets if the Western powers are willing to reach agreement to ban atomic and hydrogen weapons, to end tests thereof, and to liquidate foreign military bases in other nations' territories. In that case, an agreement on the use of outer space for peaceful purposes only would unquestionably meet no difficulties."

Apparent causes were instabilities in the torque sensor circuit and the pitch-free floating gyro device. The upper stages and payload broke up on re-entry into the atmosphere over the Pacific.

At Chkalovskiy Airfield, the Vykhod airlock experiments are repeated, this time to an altitude of 37 km. This time the tests, run at up to 37 km equivalent altitude, are successful. The cosmonaut's pulse reached 90-108 per minute during the effort to get into the lock and open it. In all the test took two hours, but Korolev was pleased with the results. But afterwards he differs with Kamanin in the need for a 16-m arm centrifuge to be used for cosmonaut training. It should mainly be used by industry, Korolev believes.

Orbiting Solar Observatory; returned solar X-ray, UV, gamma ray data. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).

Environmental Survey Satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

VVS Party Conference. It is clear to Kamanin that there is no support from the Air Force for manned spaceflight. Kamanin only heard yesterday that Babakin is working on an automatic soil sample return spacecraft. He will need a minimum of two to three years to complete it. Kamanin complained that it would interfere with plans for the L1 program. An uninterrupted series of flights will be needed to complete the L1 spacecraft qualification, and the Ye-8, using the same booster, could be an interference in achieving that goal.

NASA Hq. released a 12-month forecast of manned space flight missions, reflecting an assessment of launch schedules for planning purposes. Five flights were scheduled for the remainder of 1969:

• Apollo 9 - February 28, SA-504, CSM 104, LM-3; manned orbital; up to 10 days' duration; Atlantic recovery.
• Apollo 10 - May 17, SA-505, CSM 106, LM-4; manned lunar mission, Pacific recovery.
• Apollo 11 - SA-506, CSM 107, LM-5; manned lunar mission; up to 11 days' duration; Pacific recovery.
• Apollo 12 - SA-507, CSM 108, LM-6; manned lunar mission; up to 11 days; Pacific recovery.
• Apollo 13 - SA-508, CSM 109, LM-7; manned lunar mission; up to 11 days' duration; Pacific recovery.

Kamanin arrives at Tyuratam at 15:30 aboard an An-24. The State Commission for the first Ye-8 robot lunar rover mission is chaired by Tyulin at Area 31. The spacecraft will make a soft landing on the moon, deploy a mobile lunar rover that can traverse slopes up to 30 degrees. The rover will find a position that is clear of obstacles for the first Soviet manned lunar landing. It will then park there, and provide a landing beacon for the LK manned lander. The spacecraft will have a mass of 1700 kg in lunar orbit. Launch is set for 19-20 February.

Leonov reports that the Tu-104 was ready last night for the flight to observe a rocket launch using the Svinets device. All went normally. The second launch will be made tonight at 20:00.

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 26 deg W in 1971-1975?; over the Americas at 105 deg W in 1976-1983; over the Americas at 110 deg W in 1983; over the Americas at 105 deg W in 1983-1998 As of 5 September 2001 located at 104.88 deg W drifting at 0.004 deg W per day. As of 2007 Mar 9 located at 105.24W drifting at 0.007W degrees per day.

Area survey photo reconnaissance satellite; returned film capsule.

Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network.

Retrieved solar camera film cartridges and external materials exposure package.

TsK and SM Decree 'On USSR-France co-operation in space' was issued.

Military navigation satellite.

Manned five crew. Deployed Westar 6, Palapa B2; tested Manned Maneuvering Unit (MMU). Payloads: PALAPA-B2 (Indonesian communications satellite) with Payload Assist Module (PAM)-D and WESTAR (Western Union communications satellite)-Vl with PAM-D. Both satellites were deployed but the PAM-D in each satellite failed to ignite, leaving both satellites in earth orbit. Both satellites were retrieved and returned to earth for renovation on the STS-51-A mission. The manned maneuvering unit (MMU) was tested with extravehicular astronauts as free flyers without tethers as far as 98 m from the orbiter. Shuttle Pallet Satellite (SPAS)-01 experiments, Monodisperse Latex Reactor (MLR), Isoelectric Focusing Experiment (lEF), Acoustic Containerless Experiment System (ACES), Cinema 360 cameras, five getaway specials (GAS), Aerodynamic Coefficient Identification (ACIP)/High Resolution Accelerom-eter Package (HIRAP).

Deployed from STS 41B 4 February 1984; failed to reach proper orbit; recovered by STS-51A. The Westar series of geostationary spacecraft provide commercial communications services for Western Union. Westar 6 failed to achieve geosynchronous orbit after being deployed from the Space Shuttle. It was later retrieved by another Shuttle mission (November 14, 1984) and returned for refurbishment and relaunch. All Westars have been launched by NASA on a reimbursable basis. Spacecraft: Westar uses the Hughes HS-376 spacecraft design. Spin stabilised with a despun antenna section. Body mounted solar cells. Once on orbit, an outer cylinder deploys downward in 'dixie-cup' fashion to increase the solar panel area. Payload: Westar spacecraft typically carried 12 to 24 transponders in the 4-6 GHz range. A single antenna reflector (72 inch diameter) is used with an array of offset feed horns. The reflector uses two polarisation-selective surfaces for horizontal and vertical polarised signals.

Deployed from STS 41B on 5 February 1984; Integrated Rendezvous Target.

Deployed from STS 41B 4 February 1984; failed to reach proper orbit; recovered by STS-51A.

German-built Shuttle Pallet Satellite (SPAS), first flown on STS-7, became first satellite refurbished and flown again. SPAS remained in payload bay due to electrical problem with Remote Manipulator System (RMS).

Defense Meteorological Satellite Program.

High resolution photo reconnaissance. Spacecraft failed. Blown up in orbit on February 27.

Global Positioning System. Placed in Plane Plane B Slot 1.

Deployed ODERACS A-F, Bremsat, carried Wake Shield Facility. Payloads: Wake Shield Facility (WSF) 1 and SPACEHAB 02. Getaway special bridge assembly experiments: Capillary Pumped Loop (CAPL), Orbital Debris Radar Calibration Spheres (ODERACS), University of Bremen Satellite (BREMSAT), G-514, G-071, and G-536. Shuttle Amateur Radio Experiment (SAREX) II; Auroral Photography Experiment (APE-B).

Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Orbital Debris Radar Calibration Sphere; deployed from STS-60.

Orbital Debris Radar Calibration Sphere; deployed from STS-60.

Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Orbital Debris Radar Calibration Sphere; deployed from STS-60. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Atomic oxygen, dust particle, microgravity, reentry experiments.

Orbital Reentry Experiment. Orbital Re-entry Experiment Vehicle (OREX) Ryusei. Acquisition of data related to atmospheric reentry. Launch vehicle H-II rocket test flight H-II 1F. Launching organization NASDA. Launch time 2220:00 UT.

Vehicle Evaluation Payload; monitored H-2 performance. Vehicle Evaluation Payload (VEP) MYOJO. Provides a ranging function as well as functions to measure the acceleration and deformation, in order to confirm the accuracy of the H-II rocket orbit injection and understand the environment of the payload equipme nt. Launch vehicle H-II rocket test flight H-II 1F. Launching organization NASDA. Launch time 2220:00 UT.

Reentered?

Deployed ODERACS 2A-2E; deployed and retrieved Spartan 204. Discovery rendezvoused with Russia's space station, Mir, to a distance of 11 m and performed a fly-around, but did not dock with Mir. Payloads: SPACEHAB 03, Shuttle Pointed Autonomous Research Tool for Astronomy (SPARTAN) 204, Cryo Systems Experiment (CSE)/GLO-2 Experi-ment Payload (CGP)/Orbital Debris Radar Calibration Spheres (ODERACS) 2, Solid Surface Combustion Experiment (SSCE), Air Force Maui Optical Site (AMOS), IMAX Cargo Bay Camera (ICBC)

Retrievable payload to observe galactic dust in far UV; deployed from STS 63 2/7/95, retrieved 2/9/95.

Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95.

Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered Sep 29

Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered?

Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered Mar 2

Orbital Debris Radar Calibration spheres; deployed from STS 63 2/4/95. Reentered Feb 27

ELINT satellite.

Spanish domestic geosynchronous communications satellite. Stationed at 30 deg W. Positioned in geosynchronous orbit at 30 deg W in 2000. As of 3 September 2001 located at 30.14 deg W drifting at 0.013 deg W per day. As of 2007 Mar 9 located at 30.01W drifting at 0.005W degrees per day.

Americom 12 satellite, also known as Worldsat 2. The first Alcatel Spacebus 4000 satellite to be launched.

Last launch of an Atlas model using the original, innovative, balloon propellant tanks conceived in 1947. Third launch of new generation paired satellites used for tracking, characterisation, and intelligence on naval vessels and civilian shipping worldwide.

Wearing Orlan suits, the crew emerged from the Pirs airlock of the station and first released a surplus Orlan suit with its radio transmitter activated, dubbed SuitSat. SuitSat broadcast greetings in six languages to radio amateurs for two orbits before its batteries failed. The crew then moved to the Zarya module and relocated the Strela crane grapple fixture to the Unity module. This cleared Zarya for the future temporary stowage of debris shields. The crew moved on to the station's center truss, where they safed a cutting mechanism on one of two umbilicals to the Mobile Transporter rail car. Returning to Pirs, they retrieved a microorganism experiment and photographed the exterior of Zvezda.