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Astronautical and Aeronautical Events of 1962 - NASA's History Office

Astronautical and Aeronautical Events of 1962 - NASA's History Office

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Oct. 20<br />

Oct. 26<br />

Oct. a7<br />

Oct. 31<br />

Nov. 1<br />

coBYos XI<br />

(U.S.S.R.).<br />

ANNA In (United<br />

States).<br />

MARE I<br />

(U.B.8.R.).<br />

Not avail-<br />

able.<br />

<strong>1962</strong> Beta-<br />

Ka Pa<br />

IW 8etahmbda<br />

I(w2 Beta-<br />

M u<br />

Not avail-<br />

able.<br />

Not avail,<br />

able.<br />

Thor-<br />

Agene.<br />

Thor-<br />

Delta.<br />

Thor-<br />

Abls<br />

Star.<br />

Not avail.<br />

able.<br />

strumentation includes vidibn camera,<br />

gamma-fay spectrometer, radar<br />

reflectivity experiment, <strong>and</strong> seismometer;<br />

3 tpusdtters; 8,880 solar cells;<br />

I silver-zmc battery; 6 silvercadmium<br />

batteries.<br />

Total weight: Not available.<br />

Objective: Continuation <strong>of</strong> Cosmos<br />

scienti0c satellite serles.<br />

Payload: Not available.<br />

Not available.<br />

Total weight: 1001bs.<br />

Objective: Inject scientific satellite<br />

into elliptic81 orbit to stud artifldsl<br />

radiation belt created by 8.5. highaltitude<br />

nuclear explosion 7/9/02.<br />

Payload: 27” I Iff’ cone wtth magnetometer<br />

boom <strong>and</strong> 4 solar paddles;<br />

experiments were on magnetic field<br />

ion-electron, electron flux, <strong>and</strong> diad<br />

hution in pitch angle <strong>of</strong> electrons’<br />

transmitter; optical attitude senso<<br />

solar cells, including solarcell damage<br />

experiment.<br />

Total weight: 360 lbs.<br />

Objective: Orbit geodeticsatellite to<br />

calibrate Instruments at U.S. tracking<br />

stations around the world <strong>and</strong> obtain<br />

geodetic data.<br />

Payload: 36” sphere, contatning 4<br />

flashing-light beacons Secor radio<br />

ranging system Dopiler radio system<br />

transmittek solar cells.<br />

Tbtsl weight: 1:980 lbs.<br />

Objective: Conduct fly-by <strong>of</strong> planet<br />

Mars. gather interplanetary data on<br />

trip to Man <strong>and</strong> Martian data on<br />

fly-by: take TV Dictum <strong>of</strong> Maa <strong>and</strong><br />

relay them to ehth.<br />

Payload: 10’ I 1Y (in cruise posftion.<br />

with solar naneh <strong>and</strong> radiatora<br />

extended) strich; -in 2 wm rtmenu.<br />

orbital compartment mntmid-cd.urse<br />

motor, solar cells, radl.<br />

atom. <strong>and</strong> antennas; planetary coma<br />

partment contains TV cameri, spee<br />

tdectometer, spectrograph m<br />

netornetem, gaa discbar e <strong>and</strong> ’kcin%<br />

lating gauges, radiOte~~pe, lowenergy-proton-electron-ion<br />

trap <strong>and</strong><br />

micrometeorite countera. Source:<br />

TasS).<br />

Instruments reported to have<br />

functioned as lanned. Information<br />

on or& status not<br />

available.<br />

Btill in orbit.<br />

Wmt into orblt with min rate 10<br />

&&thepl&ed wee. because<br />

<strong>of</strong> failure <strong>of</strong> dedpin weights to<br />

deploy; spin rate renders data<br />

fr&m the-2 electron directional<br />

detectora almost unusable. Still<br />

in orhlt, dill transmltthg.<br />

Still in orbit. All 3 tracking sys-<br />

tems on board satellite stU<br />

tmsmitting.<br />

Trip to Mars to take about<br />

7 mos. Soviet calculations in-<br />

dicated that on original trajec-<br />

tory satellfte would pass<br />

n s b mi. from am. NO<br />

micieourse wmtion reported<br />

<strong>of</strong> 12/31/02. Still transmit-<br />

-.

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