The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
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Thagard, Norman E. (1943–)<br />
An American astronaut and a veteran <strong>of</strong> five spaceflights<br />
(including the first by an American on Soyuz) who, in<br />
1994–1995, set a new U.S. space endurance record <strong>of</strong> 115<br />
days during his stay aboard Mir (the previous record <strong>of</strong><br />
84 days having been held by the crew <strong>of</strong> Skylab 4). Thagard<br />
received a B.S. (1965) and an M.S. (1966) in engineering<br />
science from Florida State University and a<br />
doc<strong>to</strong>r <strong>of</strong> medicine degree from the University <strong>of</strong> Texas<br />
Southwestern Medical School in 1977 and was on active<br />
duty with the Marine Corps Reserve from 1966 <strong>to</strong> 1971,<br />
rising <strong>to</strong> the rank <strong>of</strong> captain. Selected as an astronaut candidate<br />
by NASA in 1978, he served as a mission specialist<br />
on Shuttle flights STS-7 (1983), STS-51B (1985), and<br />
STS-30 (1989), the payload commander on STS-42<br />
(1992), and the cosmonaut/researcher on the Russian Mir<br />
18 mission (1995).<br />
THEMIS (Time His<strong>to</strong>ry <strong>of</strong> Events and Macroscale<br />
Interaction during Subs<strong>to</strong>rms)<br />
A proposed mission <strong>to</strong> study the onset <strong>of</strong> magnetic<br />
s<strong>to</strong>rms within the tail <strong>of</strong> Earth’s magne<strong>to</strong>sphere. It<br />
would fly five microsatellite probes through different<br />
regions <strong>of</strong> the magne<strong>to</strong>sphere and observe the origin and<br />
evolution <strong>of</strong> s<strong>to</strong>rms. Led by Vassilis Angelopoulos <strong>of</strong> the<br />
University <strong>of</strong> California, Berkeley, THEMIS is one <strong>of</strong><br />
four MIDEX (Medium-class Explorer) missions selected<br />
by NASA in April 2002 for further development, two <strong>of</strong><br />
which will be selected for launch in 2007 and 2008.<br />
thermal barrier<br />
<strong>The</strong> speed at which frictional heat, generated by the rapid<br />
passage <strong>of</strong> an object through the atmosphere, exceeds<br />
endurance compatible with the function <strong>of</strong> the object.<br />
thermal load<br />
Stresses imposed upon a spacecraft or launch vehicle due<br />
<strong>to</strong> expansion or contraction (or both) <strong>of</strong> certain structural<br />
elements when exposed <strong>to</strong> a wide range <strong>of</strong> temperatures.<br />
thermionic<br />
Operating by means <strong>of</strong> electrically charged particles emitted<br />
by an incandescent material.<br />
thermodynamics<br />
<strong>The</strong> study <strong>of</strong> the relationship between heat and mechanical<br />
energy.<br />
thermosphere<br />
An upper part <strong>of</strong> Earth’s atmosphere that includes the<br />
ionosphere and extends from an altitude <strong>of</strong> 85 km<br />
(above the mesopause), where the temperature is about<br />
−33°C, <strong>to</strong> the lower level <strong>of</strong> the exosphere at 500 km,<br />
Thor 433<br />
where the temperature is about 1,500°C. <strong>The</strong> thermosphere<br />
is known <strong>to</strong> be very active with waves and vertical<br />
tides <strong>of</strong> thin air far above the highest clouds and s<strong>to</strong>rms<br />
<strong>of</strong> charged particles. However, it is still poorly unders<strong>to</strong>od<br />
and is difficult <strong>to</strong> explore. Weather balloons and<br />
research aircraft cannot reach it. Sounding rockets do<br />
travel through the upper atmosphere—however, they can<br />
at best take short snapshots <strong>of</strong> a specific region, and they<br />
do not provide global mapping. Furthermore, the Space<br />
Shuttle orbits in a region well above the lower thermosphere<br />
and passes through it only briefly during reentry.<br />
A promising alternative approach is <strong>to</strong> tether a probe<br />
from a larger orbiting platform and then lower the probe<br />
in<strong>to</strong> the region <strong>of</strong> the thermosphere (see space tether).<br />
<strong>The</strong> feasibility <strong>of</strong> this technique has already been demonstrated<br />
by NASA’s SEDS experiments.<br />
Thiel, Walter (1910–1943)<br />
A German engineer who directed the development <strong>of</strong> the<br />
V-2 (A-4) rocket mo<strong>to</strong>rs (see “V” weapons). His designs<br />
resulted in a leap from engines that developed a few<br />
thousand kilograms <strong>of</strong> thrust <strong>to</strong> engines that were more<br />
than ten times as powerful. Thiel and his family were<br />
killed during the Allied attack on Peenemünde when<br />
their shelter <strong>to</strong>ok a direct hit from a falling bomb.<br />
Thor<br />
An intermediate-range ballistic missile (IRBM) that was<br />
adapted for use as a space launch vehicle and is the direct<br />
ances<strong>to</strong>r <strong>of</strong> the Delta rocket family.<br />
Development <strong>of</strong> the Thor was authorized in November<br />
1955 <strong>to</strong> give the U.S. Air Force an independent<br />
IRBM capability. At the time, the Army Ballistic Missile<br />
Agency (ABMA) was already developing the Reds<strong>to</strong>ne<br />
medium-range ballistic missile and the Jupiter IRBM.<br />
Since the Air Force was now free <strong>to</strong> compete with the<br />
Army in creating a similar weapon, an intense rivalry<br />
broke out between the two services. <strong>The</strong> Air Force<br />
requested proposals for a missile capable <strong>of</strong> carrying a<br />
nuclear warhead at least 2,400 km—the distance from<br />
England <strong>to</strong> Moscow. <strong>The</strong> Douglas Aircraft Company<br />
came up with a design that used the warhead and guidance<br />
system already being developed for the Atlas and<br />
the engine from the Navaho. <strong>The</strong> resulting missile could<br />
fit inside a Douglas C-124 Globemaster II for easy transportation<br />
<strong>to</strong> a launch site. <strong>The</strong> first Thor was ready <strong>to</strong> fly<br />
in August 1956, and the first operational Thors were<br />
deployed in England by the end <strong>of</strong> 1958.<br />
Two-thirds <strong>of</strong> the Thor’s body held the liquid propellants—liquid<br />
oxygen and RP-1—for the missile’s singlestage<br />
engine, whose thrust capability was similar <strong>to</strong> that<br />
<strong>of</strong> both the Jupiter IRBM engine and each individual<br />
Atlas ICBM booster stage engine. Two vernier engines,