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

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158 Genesis<br />

launch failed and the vehicle fell in<strong>to</strong> the ocean. It<br />

was replaced by a backup called the Augmented Target<br />

Docking Adapter (ATDA), which was not a modified<br />

Agena but simply a TDA with a cylindrical back<br />

Genesis<br />

A NASA mission that will collect 10 <strong>to</strong> 20 micrograms<br />

<strong>of</strong> particles from the solar wind using high purity wafers<br />

set in winglike arrays—the agency’s first sample-return<br />

attempt since <strong>Apollo</strong> 17 in 1972. For two years, Genesis<br />

will orbit around the first Lagrangian point (L1) <strong>of</strong> the<br />

Earth-Sun system before returning <strong>to</strong> enable recovery <strong>of</strong><br />

its 210-kg sample capsule in September 2004. As the capsule<br />

descends by parachute, it will be caught by a helicopter<br />

over the Utah desert. Scientists know that the<br />

Solar System evolved a little under five billion years ago<br />

from an interstellar cloud <strong>of</strong> gas, dust, and ice, but the<br />

exact composition <strong>of</strong> this cloud remains unknown. As<br />

its name implies, Genesis will help unravel this mystery<br />

by recovering material that has been shot out <strong>of</strong> the<br />

upper layers <strong>of</strong> the Sun—material that has not been modified<br />

by nuclear reactions in the Sun’s core and is thus<br />

representative <strong>of</strong> the composition <strong>of</strong> the original presolar<br />

nebula. At its stable location at the L1 point, Genesis<br />

will be well outside Earth’s magne<strong>to</strong>sphere, which<br />

deflects the solar wind away from the terrestrial environs.<br />

Launch<br />

Date: August 8, 2001<br />

Vehicle: Delta 7326<br />

Site: Cape Canaveral<br />

GEO<br />

An acronym for either geostationary Earth orbit (see geostationary<br />

orbit) or geosynchronous Earth orbit (see geosynchronous<br />

orbit).<br />

Geo-IK<br />

A Soviet geodetic satellite system, also known as Musson<br />

(“monsoon”). <strong>The</strong> first Geo-IK was launched in 1981, <strong>to</strong><br />

be followed by roughly one more per year until the mid-<br />

1990s. Normally one or two satellites were operational at<br />

any given time. Each 1,500-kg Geo-IK was launched by a<br />

Tsyklon-3 from Plesetsk and placed in<strong>to</strong> an almost circular<br />

low Earth orbit with an average altitude <strong>of</strong> 1,500 km<br />

and an inclination <strong>of</strong> 73.6° or 82.6°. In contrast, the<br />

end <strong>to</strong> mate it directly <strong>to</strong> the Atlas. Unfortunately, the<br />

ATDA’s shroud failed <strong>to</strong> separate properly, leaving it<br />

in “Angry Alliga<strong>to</strong>r” mode and unable <strong>to</strong> support the<br />

docking.<br />

Etalon geodetic satellites were placed in much higher<br />

orbits and were completely passive.<br />

geocentric<br />

Relating <strong>to</strong> or measured from Earth’s center.<br />

geodesy<br />

<strong>The</strong> science that treats the shape and size <strong>of</strong> Earth<br />

through applied mathematics.<br />

geodesy satellites<br />

Spacecraft that are used <strong>to</strong> measure the location <strong>of</strong> points<br />

on Earth’s surface with great accuracy. <strong>The</strong>ir observations<br />

help <strong>to</strong> determine the exact size and shape <strong>of</strong> Earth, act<br />

as references for mapping, and track movements <strong>of</strong><br />

Earth’s crust.<br />

GEOS (Geodetic Earth Orbiting Satellite)<br />

NASA spacecraft flown as part <strong>of</strong> the National Geodetic<br />

Satellite Program (NGSP). Instrumentation varied by<br />

mission, with the goals <strong>of</strong> pinpointing observation points<br />

(geodetic control stations) in a three-dimensional Earth<br />

center-<strong>of</strong>-mass coordinate system <strong>to</strong> within 10 m, determining<br />

the structure <strong>of</strong> Earth’s gravity field <strong>to</strong> five parts<br />

in 10 million, defining the structure <strong>of</strong> Earth’s irregular<br />

gravitational field and refining the locations and<br />

strengths <strong>of</strong> large gravity anomalies, and comparing the<br />

results <strong>of</strong> the various systems onboard the spacecraft <strong>to</strong><br />

determine the most accurate and reliable system. GEOS<br />

1 and 2 were part <strong>of</strong> the Explorer series and also designated<br />

Explorer 29 and 36. GEOS 3 was designed <strong>to</strong> be a<br />

stepping-s<strong>to</strong>ne between the NGSP and the Earth and<br />

Ocean Physics Application Program by providing data <strong>to</strong><br />

refine the geodetic and geophysical results <strong>of</strong> the NGSP.<br />

It proved important in developing gravity models before<br />

the launch <strong>of</strong> TOPEX/Posiedon since it was located<br />

near that spacecraft’s mirror inclination. (See table,<br />

“GEOS Missions.”)<br />

Geosat<br />

A U.S. Navy satellite designed <strong>to</strong> measure sea surface<br />

heights <strong>to</strong> within 5 cm. After a year-and-a-half-long<br />

classified mission, Geosat’s scientific Exact Repeat Mission<br />

(ERM) began on November 8, 1986. When the

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