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Astronautics and Aeronautics, 1967 - NASA's History Office

Astronautics and Aeronautics, 1967 - NASA's History Office

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ASTRONAUTICS AND AERONAUT1 October 19<br />

dioxide <strong>and</strong> found ionospheric observations on daytime side indicated<br />

electron density; dual-frequency radio propagation provided data on<br />

Venus mass as 81.50% of earth’s mass, <strong>and</strong> astronomical unit deter-<br />

mination agreed with radar computations; <strong>and</strong> ultraviolet photometer<br />

found hydrogen corona comparable with that of earth, detected no<br />

oxygen, <strong>and</strong> found night airglow to be very faint ultraviole emission<br />

detected at dark limb of planet-probably result of chemic8 t reactions,<br />

particle bombardment of electrical discharge. Spacecraft’s mission also<br />

Was to accumulate data on interplanetary environment during period of<br />

increased solar activity. After return to cruise mode, Mariner V would<br />

resume report on interplanetary space weather. By end of November<br />

<strong>1967</strong>, when earth was no longer in direction of high-gain antenna pat-<br />

tern, communications would be terrninated ; however, three-month-dura-<br />

tion communications would be poss?ble during next five years. (NASA<br />

Proj Off; Wilford, NYT, 10/20/67, 1; Sullivan, NYT, 10/22/67, 12)<br />

* Cone-shaped RAM C-1 spacecraft was successfully launched from NASA<br />

Wallops Station by four-stage Scout booster at 1:33 pm, EDT. On ter-<br />

mination of eight-minute ballistic flight, impact occurred 725 mi down-<br />

range about 150 nm northeast of Bermuda. Spacecraft, 15 in long <strong>and</strong><br />

26 in in dia with 12-in-dis hemisphere nose, plunged back into earth‘s<br />

atmosphere at 17,000 mph in flight test to study methods for preventing<br />

loss of radio signals from reentering spacecraft. No recovery was<br />

attempted.<br />

NASA’s Project RAM (Radio Attenuation Measurement) was to meas-<br />

ure effectiveness of water addition concept in maintaining communica-<br />

tions during reentry. Additional experiments were also included to<br />

evaluate X-b<strong>and</strong> telemetry system as a means of overcoming blackout J<br />

study plasma <strong>and</strong> ablation effects on antenna performance; measure<br />

attenuation as a €unction of signal frequency; <strong>and</strong> obtain measurements<br />

of ion densities in the flow field of the spacecraft in the presence of abla-<br />

tion <strong>and</strong> water injection.<br />

Water was injected at three points on spacecraft-on nose cap <strong>and</strong> on<br />

each side-with nitrogen gas as pressurizing agent. Ion density changes,<br />

due to varying amounts of water injection, were measured. X-b<strong>and</strong> fre-<br />

quency experiment showed blackout period of communications was<br />

reduced by 6 sec, using water-injection method.<br />

Series of Arcasonde meteorological rockets were launched from Ber-<br />

muda before <strong>and</strong> after RAM C-1 experiment to collect upper atmosphere<br />

density, temperature, <strong>and</strong> wind data. (NASA Proj Off; NASA Release 67-<br />

261 ; WS Releases 67-33,67-34)<br />

NASA Aerobee 150 sounding rocket launched from WSMR reached 118-mi<br />

(182-km) altitude in flight to observe profile of solar hydrogen Lyman-<br />

alpha line <strong>and</strong> to measure radiation in relation to earth’s planetary hy-<br />

drogen. Experiments performed satisfactorily, but range schedule delay<br />

caused loss of coordination with Mariner V experiment. (NASA Rpt SRL)<br />

NASA Arcas sounding rocket was launched from Barking S<strong>and</strong>s, Hawaii, to<br />

36-mi (58-km) altitude, fifth in NOTS series of seven to measure incident<br />

solar uv irradiance in support of Ogo ZV’s mission. Excellent data were<br />

obtained. Rocket <strong>and</strong> payload performed satisfactorily. (NASA Rpt SRL)<br />

0 USAF F-111A aircraft crashed near Bowie, Texas; two crew members<br />

ejected safely in detachable cockpit. According to General Dynamics<br />

Corp. pilots David Thigpen <strong>and</strong> Max Gordon, aircraft had faulty hy-<br />

draulic system which made maneuvering impossible. Crash was second<br />

324-801 0-49-21 311

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