The R-3 3000 km range missile and R-3A subscale technology demonstrator were cancelled. As a replacement work was to start on the R-5 and R-11. The missiles originated as Theme N-2 of the R-3 project. This was an alternate approach to delivering nuclear warheads on West European targets - road-mobile or sub-launched missiles of shorter range with lighter warheads that could be launched from forward areas and reach enemy targets.

Jupiter missile Live System Test 217, the first to be fired under simulated tactical conditions using GSE prescribed for the Jupiter deployed to NATO I, was fired from AMR at 1102 hours EST. The missile successfully accomplished all primary and secondary missions. The nose cone impacted 1.1 nm over and 0.2 nm right of the pre-determined target 962.5 nm downrange.

Carried military experiments to test communications and navigation equipment needed for command and control of Soviet nuclear forces (later used on the Uragan navigation satellites). Also conducted operational monitoring of cosmic rays, radiation from nuclear tests, and natural and artifically-produced radiation belts.

Test of the Los Alamos XW-50X1 60 kiloton nuclear warhead. Launch vehicle was a solid propellant XM-33 Strypi rocket with a Recruit booster stage. The warhead detonated at an altitude of 147 km, 66 km from Johnston Island. Observers on the island saw a green and blue circular region surrounded by a red ring. This faded in less than a minute. Blue-green streamers and pink striations developed that lasted half an hour. At this yield, even with the high altitude, extensive disruption of communications were not reported.

The traditional meeting with the crew is followed by a smaller group in Korolev's office. Numerous toasts are drunk to the crew, to future victories in space, and... "on to the moon". From 18:00 to 20:00 the cosmonauts are prepared by Keldysh, Tyulin, Pashkov, Skuridin, Mozzhorin, Rumyanets, and others in allowable answers for the next day's press conference. Kamanin wants the crew to be free to answer questions about the physical characteristics of the booster and spacecraft (thrust, weight, dimensions, and so on) but Keldysh and Tyulin prohibit it strongly.

Headquarters USAF and AFSC directed the go-ahead for Phase II of the Initial Defense Communications Satellite Program (IDCSP) with a funding ceiling of $30 million after 14 September 1964. This action approved the launch of three IDCSP payloads on Titan IIIC research and development vehicles that were to be launched in the first half of 1966.

Apollo spacecraft 009, first of the type that would carry three astronauts to the moon and back, was accepted by NASA during informal ceremonies at North American. Spacecraft 009 included a CM, SM, launch escape system, and adapter. It went to Cape Canaveral for integration with the first Saturn IB (Saturn IB and SIVB stages received August 1965). The spacecraft was stacked on the launch vehicle on 26 December.

First coordination meeting on the S-IVB Orbital Workshop and related Apollo Applications Program activities. MSC and MSFC program officials and engineers held their first coordination meeting on the S-IVB Orbital Workshop and related Apollo Applications Program experiment activities. Among the most significant results of this meeting was a request by Houston for inclusion of an artificial gravity experiment as part of the S-IVB command and service module concept of the Workshop. MSFC officials undertook to define the feasibility of such an experiment, examining several possible technical approaches (including cables a concept that MSC found less shall appealing). MSFC investigators also sought help from LaRC, where considerable work along this line had been done as part of that Center's MORL study program.

Coordination problems between the ministries in preparation of the Soyuz spacecraft. VVS and MAP have managers assigned for quality control of each system, while MOM (Afanasyev) counterpart staff are disorganised. Yet again conflicts have to be appealed to 'Cardinal' Ustinov.

ASAT interceptor. Intercepted Cosmos 248 target on second orbit. Repeatedly approached Cosmos 248, verifying primary and reserve homing and guidance systems. Destroyed itself in test of on-board destruct system. Counted as a failure by Western observers because that target was not destroyed; but this was not an objective of the test. Left 109 fragments in orbit, of which 54 were still in orbit in 1996.

The medical reports show all the cosmonauts lost 1.5 to 3.5 kg during the flight (with Filipchenko having the greatest loss). However Kamanin plays tennis with Gorbatko, Shonin, and Volkov just two days after the flight. They show no apparent ill effects of zero-G.

Mishin reviews the work and configurations of the Lox/LH2 (S and Sr) upper stages for the N1 necessary to achieve various programs. Mishin reviews the work and configurations of the Lox/LH2 (S and Sr) upper stages for the N1 necessary to achieve various programs (Mishin Diaries 2-293). Here was see evidence for several previously hinted-at but poorly-documented projects: the Lunar Orbital Station (N1+Almaz), the MAVR manned Mars-Venus-Flyby Spacecraft: AM Isaev - about speeding work on the engine 11D56. AM Lyulka - about speeding work on the engine 11D57.
1. S, Sr - LOS (lunar orbital station?) SNTV satellite for direct TV broadcasting, MAVT (MAVR?), DOS-II (later Mir).
2. S + Sr - L3M, Mavr, MKBS
3. S + S + Sp - L3M, MKBS, Mavr and others.
4. NII - DOS (20t - indecipherable) - this apparently refers to later plans to dump Chelomei's Proton vehicle and go back to the original plan to use the NII (consisting of the second and third stages of the N1) for this earth orbit payload class.
5. N1S => 110 t (the low earth payload for this version of the improved N1). (Mishin Diaries 2-293).

Final circumlunar flight; successfully recovered October 26, 1970. The announced objectives were investigations of the moon and circumlunar space and testing of onboard systems. The spacecraft obtained photographs of the earth on October 21 from a distance of 64,480 km. The spacecraft transmitted flight images of the earth for three days. Zond 8 flew past the moon on October 24, 1970, at a distance of 1,110.4 km and obtained both black and white and colour photographs of the lunar surface. Scientific measurements were also obtained during the flight. The spacecraft used a new variant of the double-dip re-entry, coming in over the north pole, bouncing off the atmosphere, being tracked by Soviet radar stations as it soared south over the Soviet Union, then making a final precision re-entry followed by splashdown at the recovery point in the Indian Ocean.

Provision of telephone and telegraph radiocommunications and transmission of television programmes. Positioned in geosynchronous orbit at 90 deg E in 1982-1984; 140 deg E in 1984-1988; 170 deg W in 1988-1989 As of 31 August 2001 located at 45.17 deg W drifting at 0.179 deg E per day. As of 2007 Mar 9 located at 146.19W drifting at 0.287W degrees per day.

Transport of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 22 Oct 1983 11:34:00 GMT. Boosted Salyut to 326 X 356 orbit on 4 Nov 1983. Undocked on 13 Nov 1983 03:08:00 GMT. Destroyed in reentry on 16 Nov 1983 04:18:00 GMT. Total free-flight time 5.11 days. Total docked time 21.65 days.

Replaced Molniya 3-21. Operation of the long-range telephone and telegraph radio communications system in the USSR; transmission of USSR Central Television programmes to stations in the Orbita network and within the framework of international cooperation.

Stationed at 35 deg E. Provision of telephone and telegraph radiocommunications and television broadcasting. Positioned in geosynchronous orbit at 34 deg E in 1988-1992; 12 deg E in 1992-1998 As of 3 September 2001 located at 8.88 deg E drifting at 0.001 deg W per day. As of 2007 Mar 11 located at 67.55E drifting at 0.412W degrees per day.

"University fight songs medley" sent as a tribute to the Mission Specialists and their undergraduate schools: 1. University of Oklahoma for Shannon Lucid, 2. University of Connecticut for Franklin Chang-Diaz, 3. State University of New York at Buffalo for Ellen Baker. CAPCOM: Tammy Jernigan

The orbit at burnout of the Centaur was 286 km x 25866 km x 27.0 degree. Modification of the orbit to a geostationary 38,300 km circular x 0.0 degree inclination was accomplished by the Marquardt R-4D liquid propellant motor on the HS-601 spacecraft. The satellite carried UHF and EHF transponders for naval communications, and a Ka-band Global Broadcast Service video relay package. Launch mass of 3200 kg dropped to 1550 kg once geostationary orbit was reached. UHF F/O F9 was placed over the Atlantic Ocean in geosynchronous orbit at 174 deg W in 1998; 22 deg W in 1999. Additional Details: here....

Military Communications satellite. Launch delayed from October 12 by spacecraft problem. The US Air Force Defense Satellite Communications System satellite was placed by the Centaur upper stage into a 148 km x 898 km x 29.3 deg parking orbit. A second burn put it into a 218 km x 35,232 km x 26.0 deg transfer orbit. The DSCS III B-11 IABS-8 apogee stage, with two Primex R4D liquid apogee engines, circularised the orbit at geostationary altitude on October 21 and then separated from the DSCS.

New residents arrived at the International Space Station Monday with the ISS Soyuz 7 spacecraft docking to the Station at 2:16 a.m. CDT (0716 GMT, 11:16am Moscow time). The arrival of Expedition 8 and a European Space Agency visiting researcher initiated a week of intense science operations and handover activities for the newest station crew, which will stay aboard the complex for nearly 200 days. Additional Details: here....

Finished Repairs to Canadarm 2 added lubricating oil to all working parts and installed a camera and replaced a degraded one, Replaced the Station's Cameras which are used to film NASA TV, Replaced a Blown Fuse on Dextre, Removed MLI from two ORUs stored on ESP2 in preparation for them to be moved by Dextre later this year. Three get ahead task were performed by the crew MLI was removed from the Pump Modules on ESP2 Bresnik almost got the second one, but time expired and he had to close the flap on the second Pump Module it will be moved on the next spacewalk, Installed the Radiator Grapple Bars delivered on SpaceX CRS2.