Just ahead of the troops the rocket team's documentation was moved in a truck convoy to the south. Kammler, Dornberger, and Von Braun hold their last meeting. In Bavaria, spring is just emerging from the snow.

AF flight 24. Pilot-check flight. Mach 1.1, during 4-cylinder run at 12505 m.

NACA flight 42. Flight for RKO film Jet Pilot. Slight engine fire but no damage.

Third glide flight. Damaged on landing. Following flight, plane returned to Bell plant for extensive modifications to landing gear system to prevent further landing accidents and for installation of its rocket engine.

Four of the eight H-1 engines of the Saturn C-1 first-stage booster were successfully static-fired at Redstone Arsenal for seven seconds.

The Marshall Space Flight Center announced that 1.640 million pounds of thrust was achieved in a static- firing of the F-1 engine thrust chamber at Edwards Air Force Base, Calif. This was a record thrust for a single chamber.

The Thiokol Chemical Corporation was selected by NAA to build the solid-fuel rocket motor to be used to jettison the Apollo launch escape tower following a launch abort or during a normal mission.

The request for a proposal on the Little Joe II test launch vehicle was submitted to bidders by a letter from MSC, together with a Work Statement. Five launches, which were to test boilerplate models of the Apollo spacecraft command module in abort situations, were called for: three in 1963 and two in 1964. - Additional details.

NASA sponsored a 1-day symposium in Washington on the results of the Mercury-Atlas 6 (MA-6) three-orbit flight of John Glenn. One of the items of particular interest was Glenn's 'fire-flies,' or luminous particles, and their possible origin.

Radiation, cosmic ray data. Decay date suspect Investigation of the upper atmosphere and outer space; development of elements in the design of space craft.

They are not against the flight of four Vostoks in 1963, though.

Prototype ABM radar target; supported developmental experiments for ABM systems.

Launched at 1965 Croatan MRF Expedition LP35 - - Latitude: 35.23 S - Longitude: 74.25 W.

Over Atlantic. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit at 28 deg W in 1965; 38 deg W in 1965-1966. As of 27 July 2001 located at 92.54 deg W drifting at 0.324 deg W per day. As of 2007 Jan 13 located at 47.74W drifting at 0.017E degrees per day.

High resolution photo reconnaissance satellite; returned film capsule

FU126 Solar corona (UV) / Ptr mission.

Launch vehicle failure left in useless orbit; communications tests.

There is, to the disappointment of Kamanin, no discussion of moving manned spacecraft management from TsUKOS to VVS.

Radiation, engineering experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Kamanin, the DOS crews, and 40 VVS specialists fly to Tyuratam. VVS medical officers have to battle outbreaks of measles, rabies, and dysentery at the cosmodrome. The crews are medically isolated in the Hotel Kosmonavt. In the evening they watch the film '300 Spartans'.

Area survey photo reconnaissance satellite; returned film capsule; separated cosmic ray experiment capsule.

Jupiter flyby December 1974; Saturn flyby September 1979. Solar system escape trajectory. Pioneer 11 was the second mission to investigate Jupiter and the outer solar system and the first to explore the planet Saturn and its main rings. Pioneer 11, like Pioneer 10, used Jupiter's gravitational field to alter its trajectory radically. It passed close to Saturn and then it followed an escape trajectory from the solar system. During its closest approach, December 4, 1974, Pioneer 11 passed to within 34,000 km of Jupiter's cloud tops. It passed by Saturn on September 1, 1979, at a distance of 21,000 km from Saturn's cloud tops. The spacecraft has operated on a backup transmitter since launch. Instrument power sharing began in February 1985 due to declining RTG power output. Science operations and daily telemetry ceased on September 30, 1995 when the RTG power level was insufficient to operate any experiments. As of the end of 1995 the spacecraft was located at 44.7 AU from the Sun at a nearly asymptotic latitude of 17.4 degrees above the solar equatorial plane and was heading outward at 2.5 AU/year. Routine tracking and project data processing operations were terminated on March 31, 1997 for budget reasons.

Replaced Cosmos 544. Possible ELINT satellite.

Area survey photo reconnaissance satellite; returned film capsule.

Possibly ASAT related. Radar calibration mission.

Manned five crew. First repair on orbit of a satellite, Solar Maximum Mission, by James van Hoften and George Nelson. Deployed LDEF. Payloads:Solar Maximum Mission (SMM) repair, manned maneuvering unit (MMU) satellite support, deployment of Long-Duration Exposure Facility (LDEF) in earth orbit free drift. LDEF contained 57 experiments and weighed about 10,000 kg. Cinema 360 and IMAX 70-mm cameras.

Long Duration Exposure Facility; deployed from STS 41C 7 April 1984; retrieved by STS-32 20 January 1990. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).

Military cartographic satellite; returned film capsule.

Eight satellites launched by a single carrier rocket.

Covered Oko constellation plane 7 - 161 degree longitude of ascending node.

Unmanned resupply vessel to Mir. It carried supplies for the Mir station and repair equipment for Mir's oxygen generators, replacement oxygen-generating 'candles' and a pair of new spacesuits. Docked with Mir at the rear Kvant module port on 8 Apr 1997 17:30:03 GMT. The Mir complex raised its orbit by 5 km on 15 Apr 1997 at 12:00 GMT, using Progress M-34's engine. Undocked on 24 Jun 1997 10:22:50 GMT. It was then used to perform a redocking test using newly developed remote-control procedures which were to replace the automatic system that Russia could no longer afford to buy from Ukraine. At 25 Jun 1997 09:18 GMT Mir commander Tsibliev was remotely commanding the approach of Progress to the Kvant module. This involved guiding the Progress via a television monitor. The Progress was difficult to see against the cloudy earth background at the time of the attempted docking. It went off course and collided with a solar array on the Spektr module and then the module itself. A large hole was made in a solar panel, one of the radiators was buckled, a hole was punched into Spektr's hull, and the module began to depressurize. This was not a slow leak - the crew heard a hissing sound and felt their ears pop. They disconnected the power cables leading from Mir to the main station and closed the hatch on the core module transfer section that led to Spektr. The Spektr module became fully depressurized, remaining docked to Mir with its docking hatch open. The loss of electrical connection between Spektr's solar panels and the main station cut the available power supply to the station, crippling its operations until later repairs reconnected the electrical lines. Tsibliev was also the pilot on a previous orbital collision, when he banged Soyuz TM-17 into Mir in Jan 1994. After the return of the crew to earth he was found to be to blame for the incident, although the fines assessed were later dismissed. The Progress M-34 cargo ship was backed to a safe distance from the station and was destroyed in reentry on 2 Jul 1997 06:31:50 GMT. Total free-flight time 9.90 days. Total docked time 76.70 days.

The crew succeeded in completing repair of the damaged Spektr solar panel. However the EVA was cut short when Mission Control in error commanded the Mir to drift. This was then misdiagnosed as a depletion of fuel of the VDU orientation engine, and the crew was ordered back into the station.

Lockheed Martin was charged with violating the Arms Export Control Act by assisting China in redesigning their apogee kick motor (EPKM) for the Asiasat-2 communications satellite. This was denied by the Chinese Foreign Ministry, which said that the EPKM was of totally indigenous design.