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The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity

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TWINS (Two Wide-angle Imaging<br />

Neutral-a<strong>to</strong>m Spectrometer)<br />

A mission consisting <strong>of</strong> two identical, widely separated<br />

satellites in high-altitude, high-inclination orbits, which<br />

will enable the three-dimensional visualization and resolution<br />

<strong>of</strong> large-scale structures and dynamics within the<br />

magne<strong>to</strong>sphere. A MIDEX (Medium-class Explorer),<br />

TWINS will extend the detailed study <strong>of</strong> energetic neutral<br />

a<strong>to</strong>ms in the magne<strong>to</strong>sphere that began with the<br />

IMAGE mission in 2000. TWINS instrumentation is<br />

essentially the same as the MENA (Medium-Energy Neutral<br />

A<strong>to</strong>m imager) instrument on IMAGE. However, the<br />

capability <strong>of</strong> TWINS <strong>to</strong> carry out stereo imaging will<br />

greatly extend understanding <strong>of</strong> magne<strong>to</strong>spheric structure<br />

and processes. <strong>The</strong> TWINS satellites are scheduled<br />

for launch in early 2003 and early 2004 in<strong>to</strong> orbits with<br />

apogees <strong>of</strong> 7.2 Earth-radii and inclinations <strong>of</strong> 63.4°.<br />

two-body problem<br />

<strong>The</strong> problem <strong>of</strong> describing the motion <strong>of</strong> two objects<br />

that are orbiting around each other. It is easily and accu-<br />

Tyuratam 451<br />

rately solved using New<strong>to</strong>n’s law <strong>of</strong> universal gravitation.<br />

<strong>The</strong> solutions are conic sections. Far more complex is<br />

the three-body problem, for which precise solutions are<br />

available only in special cases, such as that <strong>of</strong> Lagrangian<br />

points.<br />

two-stage-<strong>to</strong>-orbit (TSTO)<br />

A reusable launch vehicle that uses an air-breathing first<br />

stage and a separate, or parallel, rocket-propelled second<br />

stage. Examples include Sanger’s space plane and Boeing’s<br />

Beta. Various two-stage-<strong>to</strong>-orbit schemes are being<br />

considered as a replacement for the Space Shuttle as part<br />

<strong>of</strong> NASA’s Space Launch Initiative. See single-stage-<strong>to</strong>orbit.<br />

2001 Mars Odyssey<br />

See Mars Odyssey, 2001.<br />

Tyuratam<br />

See Baikonur Cosmodrome.

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