First flight test of Thor-Agena for KH program.

At a meeting to draft fiscal year 1962 funding estimates, the total purchase of Atlas launch vehicles was listed as 15, and the total purchase of Mercury spacecraft was listed as 26.

Little Joe 1-B (LJ-1B) was launched from Wallops Island with a rhesus monkey, 'Miss Sam,' aboard. Test objectives for this flight were the same as those for Little Joe 1 (LJ-1) in which the escape tower launched 31 minutes before the planned launch, and Little Joe 1-A (LJ-1A), wherein the dynamic buildup in the abort maneuver was too low. A physiological study of the primate, particularly in areas applying to the effects of the rapid onset of reverse acceleration during abort at maximum dynamic pressure, was also made. In addition, the Mercury helicopter recovery system was exercised. During the mission, all sequences operated as planned; the spacecraft attained a peak altitude of 9.3 statute miles, a range of 11.7 statute miles, and a maximum speed of 2,021.6 miles per hour. Thirty minutes from launch time, a Marine recovery helicopter deposited the spacecraft and its occupant at Wallops Station. 'Miss Sam' was in good condition, and all test objectives were successfully fulfilled.

The gun-launched rocket was shot at an elevation of 80 degrees and flew for 145 seconds. During its flight it rose to an altitude of 26 km and landed 11 km down range.

The primary objective of the design is to achieve docking to two spacecraft in earth orbit. Secondary objectives are the operation of scientific and military equipment from the spacecraft. Three different spacecraft, all launched by an R-7 derived booster, are required to achieve this:

• 7K spacecraft, capable of carrying three men into space and returning them to earth. The 5.5 tonne spacecraft has three modules, including the BO living module and the SA re-entry capsule
• 9K booster stage, with a fuelled mass of 18 tonnes. After docking with the 7K this is capable of boosting the combined spacecraft to earth escape velocity. The 9K is equipped with a 450 kgf main engine and orientation engines of 1 to 10 kgf. It will have 14 tonnes propellant when full loaded. Four sequential docking with a tanker spacecraft will be required to fill the tanks before the final docking with the 7K.
• 11K tanker, with a mass of 5 tonnes.

The system will conduct fuellings and dockings in a 250 km altitude parking orbit, and be boosted up to 400,000 km altitude on lunar flyby missions. The system will be ready in three years. Military variants proposed are the Soyuz-P and Soyuz-R. Each spacecraft will have 400 kg of automatic rendezvous and docking equipment. Manual docking will be possible once the spacecraft are within 300 m of each other.

Korolev still insists on an unguided landing and categorically rejects the use of wings. A parachute will deploy and slow the capsule to 10 m/s. Then a retrorocket will fire just before impact with the earth to provide a zero-velocity soft landing. Korolev still insists that spacesuits will not be carried for the crew. First test flight of the 7K, without docking, could not occur until the second half of 1964.

North American gave a presentation at MSC on the block change concept with emphasis on Block II CSM changes. These were defined as modifications necessary for compatibility with the LEM, structural changes to reduce weight or improve CSM center of gravity, and critical systems changes. (Block I spacecraft would carry no rendezvous and docking equipment and would be earth-orbital only. Block II spacecraft would be flight-ready vehicles with the final design configuration for the lunar missions.)

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

Northrop-Ventura verified the strength of the dual drogue parachutes in a drop test at El Centro, Calif. This was also the first airborne test of the new mortar by which the drogues were deployed and of the new pilot parachute risers, made of steel cables. All planned objectives were met. - Additional details.

At the request of Maj. Gen. Samuel C. Phillips, Apollo Program Director, ASPO reexamined the performance requirements for spacecraft slated for launch with Saturn IBs. MSC currently assessed that the launch vehicle was able to put 16,102 kg (35,500 lbs) into a circular orbit 105 nm above the earth. Based on the spacecraft control weights, however, it appeared that the total injected weight of the modules would exceed this amount by some 395 kg (870 lbs). - Additional details.

The 15 cosmonaut candidates have all 'graduated' from basic cosmonaut training. The highest scores were by Beregovoi, Shatalov, Gubarev, and Demin. Two days later they officially receive their cosmonaut rating, bringing the total contingent to 34, of which 9 have already been in space. With this contingent the Soviet Union will fly to the moon and man an orbital station. That is insufficient - Kamanin wants a 40-man second contingent. The new contingent will have to be absolutely healthy male specimens, no older than 32 years, under 175 cm in height and 75 kg in weight. Keldysh, Korolev, and Tyulin are against further female flights in space, despite Kamanin's insistence.

Failure.

High resolution photo reconnaissance satellite; returned film capsule

Maximum Speed - 1093 kph. Maximum Altitude - 15819 m. Flight Time - 462 sec.

Area survey photo reconnaissance satellite; returned film capsule.

KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

Development of systems for air defence and the control of outer space.

ASAT target for Cosmos 1243 and Cosmos 1258 interceptors.

Possible test of KH-12 systems. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

Successful test of the missile and control system, but conducted without the miniature homing vehicle.

Kazakh astronaut trained for flights to the Mir space station.

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

Part of the US Air Force Defense Satellite Communications System. To be stationed in geosynchronous orbit over the Pacific Ocean.

Israeli military radar/optical surveillance satellite using synthetic aperture X-band radar, with estimated 10 cm radar and 1 m optical ground resolution.