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Astronautics and Aeronautics, 1967 - NASA's History Office

Astronautics and Aeronautics, 1967 - NASA's History Office

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July 11 ASTRONAUTICS AND AERONAUTICS, <strong>1967</strong><br />

X-24A (formerly SV-5P) , NationH newest manned lifting-body vehicle,<br />

was publicly displayed <strong>and</strong> officially turned over to USAF in ceremonies<br />

at Martin Marietta Corp.’~ Baltimre plant. The 5,000-lb wingless<br />

vehicle, constructed by Martin Marietta Corp. under AFSC contract,<br />

would be air-launched from B-52 aircraft at AFFTC <strong>and</strong> would be driven<br />

by Thiokol rocket engines to higher altitudes <strong>and</strong> supersonic speeds<br />

before gliding to controlled l<strong>and</strong>ing. Flight tests would be conducted<br />

by five USAF <strong>and</strong> NASA pilots in late <strong>1967</strong> under joint NASA/USAF lifting-<br />

body program. (AFSC Release 59.67; Clark, NYT, 7/12/67, 1)<br />

0 First regular data reports of activity on sun’s “invisible hemisphere”-<br />

side visible from eaah only once every 13.5 days-were being made<br />

to ESSA’S Solar Disturbance Forecast Center in Boulder, Colo., by<br />

NASA’s Pioneer VI <strong>and</strong> VII satellites, in orbit around sun. Satellites’<br />

observations on physical characteristics of solar storms would allow<br />

continuous scientific study of solar surface <strong>and</strong> provide Apollo astronauts<br />

with additional warning time to avoid solar radiation hazards.<br />

(NASA Release 67-174)<br />

July 12: Soviet space officials hinted that they were conducting an advanced<br />

lunar exploration program <strong>and</strong> said that series of spacecraft<br />

from Luna IX through Luna XIII would not be used again, Space<br />

Business Daily reported. Officials did not elaborate on the “new material,,<br />

that would be used, but indicated that new plans would include<br />

unmanned mobility on lunar surface. (SBD, 7/12/67,42)<br />

American Security Council (ASC) released results of study prepared for<br />

House Armed Services Committee which concluded that U.S.S.R. would<br />

achieve a marked nuclear superiority over US. by 1971 unless steps<br />

were taken immediately to improve American strategic capabilities.<br />

Study, conducted by ASC’S National Strategy Committee under chairmanship<br />

of former AFSC Comm<strong>and</strong>er Gen. Bernard A. Schriever (USAF, Ret.),<br />

found that US. had “exchanged its goal of a war-winning strategic superiority<br />

for a strategy of mutual deterrence” while U.S.S.R. “is driving<br />

hard toward a goal of overwhelming superiority. . . .” Report predicted<br />

that by 1971 U.S.S.R. would have a 30,000- to 50,000-mt nuclear<br />

delivery capability, contrasting with 6,000- to 15,008mt for US., <strong>and</strong><br />

recommended a rapid arms buildup or development of an antiballistic<br />

missile system. It warned that “by placing our sole reliance for deterrence<br />

on ICBMS, POLARIS <strong>and</strong> POSEIDON missiles, <strong>and</strong> the remaining<br />

manned bomber force . . . [US.] places itself in the dangerous position<br />

of having only one option left if it is faced with a Soviet ultimatum<br />

to surrender. It must either fire its offensive nuclear weapons or give up<br />

its sovereignty. An ABM [Antiballistic Missile System] would at least<br />

strengthen the h<strong>and</strong> of the President if he is confronted with such a<br />

fateful decision, <strong>and</strong> it might stay the h<strong>and</strong> of an enemy at a critical<br />

moment. . . .” (Text; ASC News)<br />

July 12-19: “Cold flow” test series of Phoebus 2 nuclear reactor was successfully<br />

conducted at NRDS as part of NASA-AEC Project Rover program<br />

to develop a nuclear-propelled rocket. Purpose of tests was to check<br />

reactor design under gas-flow conditions <strong>and</strong> at liquid-hydrogen temperatures<br />

; measure variations in pressures, temperatures, <strong>and</strong> flow rates<br />

during simulated “start-upyy operations ; <strong>and</strong> obtain initial experience<br />

on the hook-up <strong>and</strong> test operations of Phoebus 2 reactors in test facility.<br />

Assembly used for experiments in “cold flow” tests was identical to that<br />

used in “hot” tests, except that it contained no fissionable material <strong>and</strong><br />

206

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