Space Task Group personnel visited the Atlantic Missile Range at the invitation of the Army Ballistic Missile Agency to observe a Jupiter launch vehicle firing and the procedures followed on the day preceding the firing. The group toured the blockhouse and received briefings on various recorders that might be used in the centralized control facility for Mercury-Redstone and Mercury-Jupiter flights.

Reactor-in-flight-test system (Rift) study, a part of the NASA-AEC program on nuclear rockets, was briefed by contractors at NASA headquarters.

Offutt AFB SMS 566 operational

Maximum Speed - 4441 kph. Maximum Altitude - 51700 m.

KH-2; Mission failed.

This document laid the foundation for the design of the Gemini launch vehicle by defining the concept and philosophy of each proposed subsystem.

MSFC awarded Rocketdyne a definitive contract (valued at $158.4 million) for the production of 76 F-1 engines for the first stage of the Saturn V launch vehicle and for delivery of ground support equipment.

Final mission of the Thor/Altair from Vandenberg AFB (first launch on 18 January 1965).

Ministry of General Machine Building (MOM) Decree 145ss 'On approval of the 7K-TK as transport for the Almaz station' was issued. It was decided that the 11F71 Soyuz-R space station would be cancelled and the Almaz would be developed in its place. Almaz was assigned the index number previously allocated to the Soyuz-R station, and Kozlov was ordered to hand over to Chelomei all of the work completed in relation to the station. However Kozlov's Soyuz 7K-TK ferry was to continue in development to transport crew to the Almaz.

The military has over a tonne of military experiments they want flown, which would require at a minimum manned flights of Voskhod s/n 6, 7, 8, and 9. Development of a military version of Soyuz is proceeding slowly. It would be best to use these existing spacecraft to fly these experiments as soon as possible, but MOM and OKB-1 have decided only to complete spacecraft s/n 6 and 7.

Thermal control experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Optical radiation test. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Ministry of Defence Decree 'On formation of Anti-Space and Anti-Missile Forces of the Air Defence Forces (PKO) to operate General Soviet ASAT systems' was issued.

KH-4A. Satellite flown nose first, all cameras operated satisfactorily.

The Congress began in the Kremlin at 10:00. Vital questions concerning the future space program will be considered.

Acquisition of meteorological information needed for use by the weather service.

Given the on-pad explosion of the LVI-2 launch attempt, plans to crew the upper VA re-entry capsule in the next test was abandoned. LVI-3 (VA's 102P and 102L / Cosmos 997 and Cosmos 998) was launched unmanned four months behind the original schedule. Both capsules were recovered after one orbit. One source indicates that one of the capsules was 009P, on its third launch and second flight to orbit. This was said to have demonstrated the multiple re-entry capability of the heat shield and the first planned reuse of a spacecraft (Gemini 2 was refurbished and reflown as MOL-1 in the 1960's, but was not designed for that purpose).

Dual reentry test of two TKS-VA capsules. Recovered March 30, 1978 after one orbit.

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

Space shuttle main engine 2007, flight engine delivered to NSTL for acceptance test firing

Soyuz 39 landed at 11:41 GMT.

First and only landing by a shuttle at White Sands, New Mexico, after weather at Edwards did not permit landing there. STS-3 landed at 16:04 GMT.

Military navigation satellite. Replaced Cosmos 1344.

In reaction to US X-30 project, Tupolev OKB asked to start work on counterpart. By 1992 mockup completed, but solving of propulsion and inlet problems intractable without access to supercomputers.

Time 25 minutes.

Photo/digital surveillance.

Global Positioning System. Placed in Plane C Slot 3.

Small Expendable-tether Deployer System.

First launch of new EORSAT, first of at 120 degree intervals on the same orbit with a 0 degree ascending node. Ocean surveillance.

Plane 3. Ascending node 230.9 degrees.

Plane 3. Ascending node 230.9 degrees.

Plane 3. Ascending node 230.9 degrees.

Plane 3. Ascending node 230.9 degrees.

Plane 3. Ascending node 230.9 degrees.

Communications satellite. Moved from Proton M to Proton K booster. Launch delayed from November 26, 2001, and March 4, 2002. The three stage Proton booster put the DM3 upper stage and payload on a suborbital trajectory. The first DM3 burn reached a circular 160 km orbit at 1742 UTC. The second burn at 1838 UTC raised apogee to about 35800 km, and a third burn near apogee at 2339 UTC raised perigee to about 3500 km and lowered inclination to 25 deg. Blok DM3 separated from the Intelsat 903 payload at 0008 UTC on March 31. By April 5, Intelsat 903 was in a 31653 x 35817 km x 0.7 deg near-synchronous orbit. Intelsat 903 had a launch mass of 4726 kg and a dry mass around 2350 kg, and carried C and Ku band antennas. It was built by SS/Loral using a derivative of the FS-1300 platform. As of 2007 Mar 5 located at 34.50W drifting at 0.011W degrees per day.

Flight Time: 2.0 Hours. White Knight Pilot: Melvill. White Knight Copilot: Binnie. Objectives: Avionics software evaluation, launch release rehearsal and landing pattern practice.

Soyuz TMA-8 docked with the Zarya nadir port of the ISS at 04:19 GMT on April 1. It undocked from Zarya on 28 September at 21:53 GMT, with the return crew of Vinogradov, Williams and space tourist Ansari aboard. It landed in Kazakhstan at 01:13 GMT on 29 September.

A repeat of the test four days earlier, this time with a Japanese-designed scramjet. The nosecone of the rocket failed to jettison and therefore scramjet ignition was not achieved. The scramjet and second stage remains were located in the desert and recovered after only 20 minutes of searching.