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Astronautics and Aeronautics, 1967 - NASA's History Office

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March 16 ASTRONAUTICS AND AERONAUTICS, <strong>1967</strong><br />

that turned automatically to trap solar rays. (Reuters, NYT, 3/17/67,<br />

13)<br />

NASA ‘Nike-Apache sounding rocket launched from NASA Wallops Station<br />

carried 96-lb payload with joint US.-India ionosphere experiment<br />

to #-mi (142-km) altitude before impacting 100 mi downrange in the<br />

Atlantic. Purpose of flight was to prove out instrumentation <strong>and</strong> test<br />

new antenna design. Experiment, which measured electron <strong>and</strong> ion den-<br />

sities <strong>and</strong> Lyman-alpha flux in lower ionosphere with a riometer-cosmic<br />

radio noise absorption device-<strong>and</strong> a Langmuir probe, was being de-<br />

veloped for series of cooperative NASA-INCOSPAR launches from Thumba<br />

range, India. (NASA Release 67-61; WS Release 67-8)<br />

* NASA Aerobee 150 sounding rocket launched from WSMR carried NRL-<br />

instrumented payload to 120-mi (193-km) to obtain spectra from a<br />

stellar ultraviolet image converter spectrograph <strong>and</strong> stellar photometric<br />

data from two ultraviolet photon counters. Rocket <strong>and</strong> instrumentation<br />

performed satisfactorily. (NASA Rpt SRL)<br />

* 110 scientists from US. <strong>and</strong> six other countries were selected by NASA<br />

Associate Administrator for Space Science <strong>and</strong> Applications Dr. Homer<br />

E. Newell-upon recommendation of Space Science Steering Commit-<br />

tee-to conduct experiments with first lunar samples returned by US.<br />

Apollo astronauts. Principal US. investigators represented 21 univer-<br />

sities, two industrial firms, three private institutions, <strong>and</strong> 10 Government<br />

laboratories. Nine scientific institutions were represented in U.K. ;<br />

three in West Germany; <strong>and</strong> one each in Canada, Japan, Finl<strong>and</strong>, <strong>and</strong><br />

Switzerl<strong>and</strong>. Most investigations would be conducted in scientists’ own<br />

laboratories, but time-critical experiments would be carried out in<br />

MSC’S Lunar Receiving Laboratory during quarantine period-antici-<br />

pated to last 30 days. Plans called for a total of 122 experiments on<br />

approximately 50 lbs of lunar material to study composition of lunar<br />

surface <strong>and</strong> search for evidence of its origin. Four major investiga-<br />

tive areas were: (1) mineralogy <strong>and</strong> petrology; (2) chemical <strong>and</strong><br />

isotope analysis; (3) physical properties; <strong>and</strong> (4) biochemical <strong>and</strong><br />

organic analysis. (NASA Release 67-55)<br />

* Francis J. Sullivan <strong>and</strong> Dr. Hermann H. Kurzweg of NASA <strong>Office</strong> of Ad-<br />

vanced Research <strong>and</strong> Technology testified before House Committee on<br />

Science <strong>and</strong> <strong>Astronautics</strong>’ Subcommittee on Advanced Research <strong>and</strong><br />

Technology. Sullivan, Director of Electronics <strong>and</strong> Control Div., said that<br />

the development of technology for high-resolution, 60- to 120-in space<br />

telescopes for optical astronomy, communications, <strong>and</strong> other potential<br />

applications was a major OART effort. “Success in this research will<br />

provide the capability to study celestial objects which cannot be viewed<br />

from the ground because of atmospheric attenuation <strong>and</strong> will provide<br />

vastly improved resolution over that attainable through the earth‘s<br />

atmosphere.”<br />

Sullivan said because environmental, structural, <strong>and</strong> control problems<br />

of large mirrors in space were almost insurmountable with conventional<br />

fabrication <strong>and</strong> alignment, unique approaches were being studied. One<br />

was 24-in-dia, three-segment mirror feasibility model in which distortion<br />

sensor, located in front of primary mirror, determined which segments<br />

were out of alignment <strong>and</strong> to what degree. Electronic circuitry then proc-<br />

essed <strong>and</strong> used the alignment data to realign mirror surface segments<br />

with actuators located behind each segment.<br />

Dr. Kurzweg, Director of Research, said the JPL had developed a<br />

new mathematical approach for calculating energy requirements for<br />

78

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