First of 9 rockets of first test series. Veered 51 degrees from flight path.

After five years of wrangling, and secret talks in Geneva between the Red Chinese and US governments, Tsien is deported from the United States. Upon arrival in China, he was immediately put to work as head of the Chinese missile program. He had to introduce US systems engineering approaches to Chinese engineers, and build the technical infrastructure to enable China to build rockets.

NACA flight 21. Stability and control with ventral fins and a new stabilizer bell crank permitting greater stabilizer travel.

A joint National Aeronautics and Space Administration/Advanced Research Projects Agency Manned Satellite Panel was formed. This panel, with the aid of technical studies prepared by the Langley and Lewis Research Centers and assistance from the military services, drafted specific plans for a program of research leading to manned space flight.

Missile test failure. Missed aimpoint by 990 m.

First Transit test satellite; failed to reach orbit.

First flight for X-15 # 2. First powered flight. Maximum Speed - 2241 kph. Maximum Altitude - 15954 m. Turbopump case failure resulted in fire in engine compartment.

NASA invited 36 companies to bid on a contract to produce the first stage of the advanced Saturn launch vehicle. Representatives of interested companies would attend a pre-proposal conference in New Orleans, La., on September 26. Bids were to be submitted by October 16 and NASA would then select the contractor, probably in November.

KH-3; film capsule recovery failed. Mission failed. Power failure and loss of control gas on orbit 33.

KH-4; film capsule recovered 1.1 days later; ERS-2 subsatellite failed to deploy. Capping shutter malfunction, slight corona and radiation fog.

Belyaev, Komarov, Shonin, Khrunov, Zaikin, Gorbatko, Volynov, and Leonov are assigned.

The Electrical Interface Integrated Validation and Joint Guidance and Control Test was completed September 21. The spacecraft/GLV Joint Combined Systems Test was run September 23. GLV tanking test was performed September 29 and the Flight Configuration Mode Test October 1, completing systems testing for Gemini-Titan 6.

Military-Industrial Commission (VPK) Decree 'On creation of a commission to compare the UR-700-LK-700 and the N1-L3' was issued.

First attempted orbital Fractional Orbital Bombardment System test. The second stage of the booster placed the third stage and dummy warhead into a 214 km x 523 km parking orbit. altitude. The third stage was evidently wrongly oriented, and instead of braking the warhead into an impact at Kapustin Yar, boosted it into a higher 280 km x 1,010 km orbit. The dummy warhead seperated but was commanded to self destruct, resulting in over 100 catalogued orbiting objects.

Development of the LK-700 manned lunar landing spacecraft was undertaken in accordance with decree 1070-363 of the Soviet Ministers and Central Committee of the Communist Party on 17 September 1967 and MOM decree 472 of 28 September 1967. Study index number 4855CC by TsNIIMASH in 1966 showed that any development of improved versions of the N1 would be practically equivalent to design and qualification of a new rocket, while the UR-700 modular approach allowed a range of payloads without requalification. The UR-700/LK-700 combination could support the DLB lunar base better, as well as Venus/Mars manned flybys and Mars landing expeditions. Work would continue through the mock-up stage until 1974.

It is decided to orient Zond 5 using the earth sensor. This is not as accurate as the star tracker, but it is good enough to ensure the spacecraft can be put on a course that will take it back to earth. However it is not accurate enough to allow a a lifting re-entry with a double skip manoeuvre and landing in the Soviet Union. It means the spacecraft must follow a high-G ballistic re-entry and land in the Indian Ocean. Afanasyev is personally supervising the midcourse orientation and engine burn.

Kamanin works with the authors of a new Gagarin book.

Area survey photo reconnaissance satellite; returned film capsule.

The basic 37K design consisted of a 4.2 m diameter pressurised cylinder with a docking port at the forward end. It was not equipped with its own propulsion system. The original authorisation was for a total of eight 37K's of various configurations. Of these, only the 37K-E (Kvant module of Mir) and the 37KS (instrumentation module in Buran) would fly.

Photo surveillance; returned film capsule.

Docked with Salyut 7. Transported a crew comprising ship's commander V V Vasyutin, flight engineer G M Grechko and cosmonaut-researcher A A Volkov to the Salyut-7 orbital station to conduct scientific and technical studies and experiments. Grechko returned in Soyuz T-13 on 25 September 1985 - emergency return.

Military cartographic satellite; returned film capsule.

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

High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission.

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.

EORSAT, first of three to be stationed at 120 degree intervals on the same orbit with a 215 degree ascending node. However cutbacks in program resulted in the constellation not being completed. Ocean surveillance.