From 1919 to 1930 he resumed full-time teaching at Clark University, and could devote only spare time and summers to rocket research.

Bell flight 1. First glide flight of AAF-NACA XS-1 rocket research airplane (No.1 of the original three X-1's built), by Jack Woolams, Bell Aircraft test pilot, at Pinecastle Army Air Base, Fla.

Launched at 2037 hours EST from AMR. The flight was successful. Actual range was 61.6 nm; 400 meters left; and 0.21 nm over the intended impact point. The primary objective was to test the accuracy of the guidance system when the missile is fired in a short range trajectory at an extreme attitude to range ratio. The missile closely followed the predicted trajectory for a successful flight which terminated 70 meters beyond and 360 meters to the Left of the expected impact point at 61.553 nm range. The short range trajectory was programmed with an extreme altitude-to-range ratio so the guidance system would be subjected to the most difficult short range expected in future tactical application. Missed aimpoint by 400 m.

NASA signed a definitive contract with Rocketdyne Division, NAA, for $102 million covering the design and development of a single-chamber, liquid-propellant rocket engine in the 1- to l.5-million-pound-thrust class (the F-1, to be used in the Nova superbooster concept). NASA had announced the selection of Rocketdyne on December 12.

Missile test failure. Missed aimpoint by 1,189 m.

After evaluating preliminary design studies, NASA selected the Hughes Aircraft Company to build seven Surveyor spacecraft. This 750-pound, three-legged, unmanned spacecraft would carry 200 pounds of instruments, including zoom television cameras, a drill to sample the lunar soil, chemical analysis equipment, and a seismometer. The first Surveyor was scheduled to be launched in 1963.

The Marshall Space Flight Center awarded contracts to the Douglas Aircraft Company and Chance Vought Corporation to study the launching of manned exploratory expeditions into lunar and interplanetary space from earth orbits.

NASA assigned George M. Low to the position of Deputy Director of MSC. He would replace James C. Elms, who had resigned on January 17 to return to private industry. Although Low continued as Deputy Associate Administrator for Manned Space Flight at NASA Headquarters until May 1, he assumed his new duties at MSC the first part of February.

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

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

The study of 325 missile countdowns, 205 missile launches, as well as all Titan scrubs and holds, indicated that GLV launching would be considerably improved and a great many scrubs precluded by the addition of such holds.

Defense Meteorological Satellite Program. Launch date was January 18, 1965. The launch was successful and correct orbit was achieved. However, the heat shield on the second stage did not deploy correctly and the mission objectives were not fully realized. This first Burner I bird is distinguishable in photos by its black second stage.

During the countdown for Gemini-Titan (GT) 2, the fuel cell hydrogen inlet valve failed to open. Efforts to correct the problem continued until it was determined that freeing the valve would delay the countdown. Work on the fuel cell ceased, and it was not activated for the flight. The fuel cell installed in spacecraft No. 2 was not a current flight design. When fuel cell design was changed in January 1964, several cells of earlier design were available. Although these cells were known to have some defects, flight testing with the reactant supply system was felt to be extremely desirable. Accordingly, it was decided to fly the entire system on GT-2, but only on a "non-interference with flight" basis. When it became clear that correcting the problem that emerged during the GT-2 countdown would cause delay, fuel cell activation for the flight was called off.

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

Not identified as a subsatellite ferret by McDowell.

Area survey photo reconnaissance satellite.

In 1967, the average cosmonaut who had already flown in space spent 50 days on public relations activities and tours - a serious loss to them in terms of training for future missions.

Possible navigation satellite.

At 10:00 a State Commission convenes at Area 17. The mistakes made during the Soyuz 4/5 flight are reviewed. The EVA began with a closed valve on Khrunov's suit. The film camera was not activated, resulting in loss of one of the key propaganda points of the exercise.

Maximum Speed - 1398 kph. Maximum Altitude - 26410 m. Flight Time - 410 sec.

Kamanin notes that interest of the leadership in manned spaceflight has collapsed with the end of the moon race. Brezhnev has declared that his primary interest is in earth orbital space stations. Both Mishin and Chelomei have stations in development, but the work is progressing slowly. There will be no launch of either of their projects until 1972 - which means the Soviets will be beaten by the US Skylab. Kamanin believes the Americans can never be beaten in space unless all space projects are guided firmly by a single Ministry of Defence and Civilian Space office. Meanwhile the Hong Kong flu epidemic is hitting many at the cosmodrome - Moroz, Popovich, and Bykovsky are all seriously ill.

MSFC began implementation of a plan for preparation and storage of unassigned Saturn hardware, phaseout of the Saturn V production capability, and amendment of the facility operations contract at the Michoud Assembly Facility for minimum surveillance of stored hardware.

Partial Failure. Failed to reach planned orbit.

Central Committee of the Communist Party and Council of Soviet Ministers Decree 46-13 'On course of work on Almaz and the TKS' was issued.

Eight satellites launched by a single carrier rocket.

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

STS-54 landed at 13:33 GMT.

The only decoy used was the single large balloon from the previous tests. Smaller balloons originally had been planned to be a part of IFT-4, but were dropped in an attempt to simplify the test.

Unsuccessful ABM test. First end-to-end system test (intercept attempt) using NMD prototype elements (except the IFICS) and range assets to approximate the objective system. The EKV was again successfully delivered by a surrogate booster and separated into the deployment basket. The failure to intercept was directly traceable to the cryogenic cooling system of the EKV, which failed to cool the IR sensors down to their operating temperatures in time because of an obstructed cooling line.

Last robotic mission to an unexplored planet in our solar system. New Horizons was due to receive a gravity boost from Jupiter in February 2007, then fly by Pluto in 2015. During launch toward Jupiter it reached a higher velocity than any manmade object, and was the first to be boosted directly to solar escape velocity. The trajectory had a perihelion of 0.98 AU, an inclination of 0.87 deg and an eccentricity of 1.03. After the Jupiter encounter it was to have a perihelion of 2.2 AU, an inclination of 2.3 deg and an eccentricity of 1.40. At encounter with Pluto on July 14, 2015, the spacecraft would be 1.1 AU above the ecliptic plane and 32.9 AU from the Sun, leaving the solar system toward the star Xi Sgr.