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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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quantum mechanics<br />

A major branch <strong>of</strong> modern physics concerned with the<br />

way matter and energy behave on a very small scale.<br />

quantum vacuum<br />

“Empty space,” when seen at the suba<strong>to</strong>mic level, is far<br />

from empty; instead, it seethes with energy, the rapid<br />

appearance and disappearance <strong>of</strong> all sorts <strong>of</strong> elementary<br />

particles, and fluctuations in the fabric <strong>of</strong> space-time<br />

itself. It is the subject <strong>of</strong> the Quantum Vacuum Forces<br />

Project and the source <strong>of</strong> zero point energy, which is<br />

seen as a potential basis for radically new forms <strong>of</strong><br />

propulsion in the far future. 256<br />

Quantum Vacuum Forces Project<br />

A project, sponsored by the Breakthrough Propulsion<br />

Physics Program, <strong>to</strong> study ways <strong>of</strong> influencing the energy<br />

density <strong>of</strong> the quantum vacuum with a view <strong>to</strong> possible<br />

applications in spacecraft propulsion. It is being conducted<br />

by a team <strong>of</strong> scientists from various academic and<br />

corporate institutions in the United States and Mexico.<br />

quasistationary orbit<br />

An orbit that is almost, but not quite, a geostationary<br />

orbit (GSO). In a quasistationary orbit, a satellite does<br />

not hang still relative <strong>to</strong> Earth, but moves in a complex<br />

elliptical trajec<strong>to</strong>ry. As seen from the ground, the path <strong>of</strong><br />

the satellite has the form <strong>of</strong> a closed intersecting loop,<br />

elongated along the horizon, and having angular dimensions<br />

<strong>of</strong> around 30° in azimuth and 5° <strong>to</strong> 6° in elevation.<br />

Quasistationary orbits <strong>of</strong>fer a number <strong>of</strong> advantages for<br />

carrying out reconnaissance (spy) tasks, including a large<br />

moni<strong>to</strong>ring area and the possibility <strong>of</strong> taking multiposition<br />

bearings on radio emitters <strong>to</strong> pinpoint their location.<br />

<strong>The</strong>y were first proved out by the Canyonseries and have<br />

Q<br />

333<br />

become a characteristic feature <strong>of</strong> American SIGINT<br />

(signals intelligence) satellites. In distinction <strong>to</strong> a GSO,<br />

which has an altitude <strong>of</strong> 35,800 km and an inclination <strong>of</strong><br />

0°, quasistationary orbits used by SIGINT satellites have<br />

a perigee (low point) <strong>of</strong> 30,000 <strong>to</strong> 33,000 km, an apogee<br />

(high point) <strong>of</strong> 39,000 <strong>to</strong> 42,000 km, and an inclination<br />

<strong>of</strong> 3° <strong>to</strong> 10°.<br />

QuikScat (Quick Scatterometer)<br />

A satellite, built under a NASA rapid delivery contract,<br />

that carries the SeaWinds scatterometer for remote sensing<br />

<strong>of</strong> ocean winds. QuikScat is among the first missions<br />

in NASA’s EOS (Earth Observing System).<br />

Launch<br />

Date: June 20, 1999<br />

Vehicle: Titan II<br />

Site: Vandenberg Air Force Base<br />

Orbit: 804 × 806 km × 98.6°<br />

QuikTOMS (Quick Total Ozone<br />

Mapping Spectrometer)<br />

<strong>The</strong> fifth launch <strong>of</strong> NASA’s TOMS instrument. TOMS-5<br />

had been scheduled <strong>to</strong> fly aboard the Russian Meteor-<br />

3M(2) satellite, but this mission was terminated in April<br />

1999. Because <strong>of</strong> the urgent need <strong>to</strong> continue daily<br />

mapping <strong>of</strong> the global distribution <strong>of</strong> atmospheric<br />

ozone, TOMS-5 was moved <strong>to</strong> a modified Microstar<br />

bus tailored for the QuikTOMS mission and procured<br />

through the Goddard Space Flight Center’s Rapid<br />

Spacecraft Development Office. It <strong>to</strong>ok <strong>of</strong>f on September<br />

21, 2001, aboard a Taurus rocket as a secondary payload<br />

alongside the OrbView-4 satellite but ended up in<br />

the Indian Ocean minutes later, after the launch vehicle<br />

malfunctioned.

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