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Astronautics and Aeronautics, 1965 - NASA's History Office

Astronautics and Aeronautics, 1965 - NASA's History Office

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ASTRONAUTICS AND AERONAUTICS, <strong>1965</strong> 21<br />

security.” (Text, Wash. Post, 1/19/65; AP, NYT, 1/19/65, 16; Norris,<br />

Wush. Post, 1/22/65)<br />

January 18: The new Sram (short-range attack missile), cited by President<br />

Johnson in his defense message to Congress, would be expected to<br />

travel 150 mi. from the launching plane to its target. The Sram<br />

would be designed for launching initially from a B-52, but later from<br />

smaller aircraft such as the F-~C or the F-111. It would be launched<br />

toward the rear after the aircraft had passed its target, would climb to<br />

100,000-ft. altitude, powered by its own solid-propellant motor, then<br />

plunge vertically toward its target having allowed the launch plane<br />

time to escape its nuclear warhead detonation. (Watson, Balt. Sun,<br />

1/19/65; Miles, Wush. Post, 1/20/65)<br />

Alfred Gessow, Chief of Fluid Physics Research, NASA, discussed before<br />

the Compressed Gas Association in New York City the problems of<br />

spacecraft deceleration <strong>and</strong> heating involved in return through the<br />

earth‘s atmosphere. He explained why the blunt shape solved deceleration<br />

<strong>and</strong> much of the heat problem in returning Mercury<br />

spacecraft from orbit through the atmosphere to earth. Looking<br />

beyond the satellite return speed (Mercury <strong>and</strong> Gemini) <strong>and</strong> lunar<br />

return speed (Apollo) , return from interplanetary flight poses the<br />

problem of much higher spacecraft speed (<strong>and</strong> thus heating). Research<br />

indicates “that the more pointed shape, although it doesn’t show<br />

up too well at the lower re-entry speeds, is better than the blunt nose at<br />

the higher speeds because the bow shock is weaker, thus producing<br />

lower radiant heating losses. Thus, in a very short time scale, but<br />

taking a big leap forward in the velocity-temperature scale, we find<br />

ourselves going into another phase of the blunt vs. pointed nose cycle.<br />

“. . . The switching between slender <strong>and</strong> blunt shapes is not new in<br />

the race for high speeds ai a! times of history. Going through<br />

history, compact rocks were replaced by slender arrows ; the concept of<br />

powder guns created round cannonballs; the rocket age produced<br />

slender forms again, which ironically, finally got blunt noses. It is<br />

interesting to see how long it took to make such changes empirically<br />

<strong>and</strong> how rapidly these variations have been made by following<br />

scientific principles. . . .”<br />

(Text)<br />

Japan expected to orbit a satellite within the next three years, New York<br />

Times reported. Although Japan’s progress in the missile field had<br />

been slowed by the limited annual budget allocations of the Defense<br />

Forces, scientific advances, particularly in the field of electronics, plus<br />

stimulus to Japanese industry provided by the Korean War, had<br />

brought marked advances in rocketry <strong>and</strong> missiles. (NYT, 1/18/65)<br />

The Communist New China News Agency (NCNA) said in a broadcast<br />

that Indonesia had successfully launched a two-stage scientific rocket<br />

Jan. 5 from somewhere in West Java. The rocket was reportedly<br />

made by the Indonesian air force. There were no other<br />

details. (UPI, Miami Her., 1/18/65)<br />

January 19: An unmanned instrument-packed Gemini spacecraft (GT-2)<br />

was launched from Cape Kennedy on Titan II launch vehicle in subor-<br />

bital shot preliminary to U.S.’s first two-man venture. Aboard was an<br />

automatic sequencer which issued orders at precise times en route to<br />

fire the rocket’s second stage, to separate the spacecraft from the rock-

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