At that time, NACA was already actively engaged in research and study of several phases. For example, in the basic studies category effort had been expended on the study of orbits and orbit control, space physical characteristics, configuration studies, propulsion system research, human factors, structures and materials, satellite instrumentation, range requirements, and noise and vibration during reentry and exit. In addition, NACA outlined the complete program covering full-scale studies of mockups, simulators, and detail designs; full-scale vertical and orbiting flights involving unmanned, animal, and manned flights and recovery; and exploitation of the program to increase the payloads. As to the design concepts for such a program, NACA believed that the Atlas launch vehicle was adequate to meet launch-vehicle requirements for manned orbital flights; that retrograde and vernier controllable thrust could be used for orbital control; that heat-sink or lighter material could be used against reentry heating; that guidance should be ground programed with provisions for the pilot to make final adjustments; that recovery should be accomplished at sea with parachutes used for letdown; that a network of radar stations should be established to furnish continuous tracking; and that launchings be made from Cape Canaveral. It was estimated that with a simple ballistic shape accelerations would be within tolerable limits for the pilot. Temperature control, oxygen supply, noise, and vibration were considered engineering development problems, which could be solved without any special breakthroughs.

Second British Black Knight rocket reached 350-mile altitude at Woomera, Australia.

Primary MSC activities for the Apollo program were relocated from Langley Field, Va., to the Manned Spacecraft Center, Houston, Tex.

North American was directed by NASA to study feasibility of using the LEM propulsion system as backup to the SM propulsion system. The most important item in the contractor's analysis was strength of the docking structure and its ability to withstand LEM main-engine and reaction control system thrusting.

Edward Z. Gray, Advanced Manned Missions Director in the Office of Manned Space Flight, asked LaRC Director Charles J. Donlan to prepare a Project Development Plan for the Manned Orbital Research Laboratory, studies for which were already underway at the Center and under contract. This plan was needed as documentation for any possible decision to initiate an orbital research laboratory project. (Gray had also asked MSC to submit similar plans for an Apollo X, an Apollo Orbital Research Laboratory, and a Large Orbital Research Laboratory.) In addition to the Project Development Plan, Gray asked for system specifications for each candidate orbital laboratory system; both of these would form the basis for a project proposal with little delay 'should a climate exist in which a new project can be started.'

The stage with the payload remained in Earth orbit as Kosmos-60.

Launched at 1965 Croatan MRF Expedition LP9 - - Latitude: 11.42 S - Longitude: 81.33 W.

Launched at 1965 Croatan MRF Expedition LP9 - - Latitude: 11.42 S - Longitude: 81.33 W.

KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Start of construction (site preparation) for Space Launch Complex 6 facilities at former Sudden Ranch property.

Tyulin and Mozzhorin review with Kamanin crewing plans. Even though the missions of Voskhod 4 and 5 are not yet clear, Tyulin wants to settle on Beregovoi and Katys for Voskhod 4, and Ponomaryova and Solovyova for Voskhod 5. Since October 1965 six crews have been in training for Soyuz flights: Gagarin -Voronov, Nikolayev-Gorbatko, Bykovsky-Matinchenko, Komarov-Kolodin, Zaikin-Khrunov, and Popovich-Artyukhin. But these are just nominal groupings, and firm crew assignments by mission have not yet been made.

Titov visits Kamanin on leave from test pilot duties at Vladimirovka. Titov will spend a year training as a test pilot on MiG-21, Su-7, and Su-9 aircraft. He flies well, and has matured and changed for the better over the last two years. Kamanin has talked to him 3 or 4 times about his future plans. Titov has bound his future with the Spiral spaceplane programme. - Additional details.

Gagarin wants better organisation of the TsPK for the L1 circumlunar manned flights, including: better training in manual navigation in case of failure of automated systems; improved training in survival of 20 G re-entries if the automated SUS capsule guidance system fails. The cosmonauts review material for the Seventh International UFO Conference in Mainz (!).

Sixth satellite of ESRO. Also registered as US object 1972-14A in A/AC.105/INF.255 with orbit 95.3 min, 525 x 548 km x 97.5 deg, category B.

High resolution photo reconnaissance satellite; returned film capsule; maneuverable.

Complete final assembly and closeout system installation.

The full engine is run at 65% power for 42.5 seconds before a fuel turbopump failure curtails the test (50 second duration planned).

Radar calibration mission.

Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 14 Mar 1979 07:19:21 GMT. Undocked on 3 Apr 1979 16:10:00 GMT. Destroyed in reentry on 5 Apr 1979 00:10:22 GMT. Total free-flight time 3.40 days. Total docked time 20.37 days.

Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 orbital station cosmonauts V V Kovalenok and V P Savinykh to carry out repairs and preventive maintenance and scientific and technical investigations and experiments.

Transmission of Central Television programmes to a network of receivers for collective use. Positioned in geosynchronous orbit at 99 deg E in 1983-1984 As of 5 September 2001 located at 6.05 deg E drifting at 18.878 deg W per day. As of 2007 Mar 9 located at 154.32W drifting at 18.879W degrees per day.

Civilian navigation satellite. Positioned in plane 12 of constellation. Maritime navigation. Signals at 150,00 MHz and 400.00 MHz. Carried COSPAS search and rescue package. Location of vessels in the Soviet merchant marine and fishing fleet; work within the international space search and rescue system for locating vessels and aircraft in distress (COSPAS-SARSAT).

After dropping away from its B-52 mothership, the X-38 deployed a ram-air parafoil, and maneuvered to a precise landing on the Edwards Air Force Base bombing range.

China, backed by Pakistan and Egypt, proposed a ban on weapons in outer space. Formal negotiations would take place via the UN Conference on Disarmament. The USA did not respond to China's proposal.

GO Kosmicheskaya Svyaz geosynchronous communications satellite, to be assigned to the Ekspress 6A slot at 80E. Replaced the first Ekspress A, lost in a launch failure in 1999. Russian satellite bus with a ommunications payload from Alcatel France. Stationed at 80 deg E. Positioned in geosynchronous orbit at 80 deg E in 2000. As of 5 September 2001 located at 80.02 deg E drifting at 0.008 deg W per day. As of 2007 Mar 10 located at 102.77E drifting at 0.018W degrees per day.

Military Technology. Sandia Multispectral Thermal Imager (MTI), aka USAF Space Test Program mission P97-3. The satellite was equipped with a hyperspectral imager for military target recognition / treaty monitoring applications.

First ICO Global Communications satellite. Lost due to launch vehicle failure; was to have entered a 10,300 km x 45 deg circular orbit. ICO's satellites would carry multiple spot beams for mobile communications.

Columbia deorbit was at 0822 UTC with landing on runway 33 at Kennedy Space Center at 0931 UTC.

ICBM Demonstration Flight - Dummy Warheads.