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

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306 ONERA (Office National d’Études et de Recherches Aérospatiale)<br />

reaching—the ultimate speed limit <strong>of</strong> light. <strong>The</strong> table<br />

(“Round-Trip Times Assuming an Acceleration <strong>of</strong> 1g”)<br />

shows some <strong>of</strong> the dramatic possibilities for lengthy<br />

excursions in a 1g spacecraft. <strong>The</strong>se figures assume equal<br />

periods <strong>of</strong> acceleration and deceleration at 1g on both the<br />

outgoing and return legs <strong>of</strong> the journey.<br />

ONERA (Office National d’Études et de<br />

Recherches Aérospatiale)<br />

<strong>The</strong> French national aerospace research center. Since its<br />

creation in 1946 it has worked on all the major French<br />

and European aeronautical and space programs, including<br />

Mirage, Concorde, Airbus, and Ariane. It operates a<br />

number <strong>of</strong> major labora<strong>to</strong>ries and wind tunnel facilities.<br />

one-way light time (OWLT)<br />

<strong>The</strong> time taken for an electromagnetic signal <strong>to</strong> travel one<br />

way between Earth and a spacecraft or another body in<br />

the Solar System.<br />

OPAL (Orbiting PicoSat Launcher)<br />

A small Stanford University satellite, launched from the<br />

JAWSAT payload adap<strong>to</strong>r on January 26, 2000, and<br />

which in turn deployed six even smaller picosatellites.<br />

Two <strong>of</strong> these picosatellites were tethered and built by the<br />

Aerospace Corporation for ARPA (Advanced Research<br />

Project Agency) research, three (<strong>The</strong>lma, Louise, and<br />

JAK) were built by Santa Clara College, and one (Stensat)<br />

was provided by radio amateurs. OPAL had a mass <strong>of</strong> 23.1<br />

kg and measured approximately 20 cm in each direction.<br />

Operation Paperclip<br />

See Paperclip, Operation.<br />

Orbcomm<br />

<strong>The</strong> first commercial venture <strong>to</strong> provide global data and<br />

messaging services; it became operational in 1998 and<br />

uses a constellation <strong>of</strong> 26 satellites in low Earth orbit. At<br />

full capacity, the Orbcomm system can handle up <strong>to</strong> 5<br />

million messages from users utilizing small portable terminals<br />

<strong>to</strong> transmit and <strong>to</strong> receive messages directly <strong>to</strong> the<br />

satellites. <strong>The</strong> system is controlled from Orbcomm’s<br />

headquarters in Dulles, Virginia.<br />

orbit<br />

<strong>The</strong> curved path an object follows under the gravitational<br />

influence <strong>of</strong> another body. A closed orbit, such as that followed<br />

by a satellite going around Earth, has the shape <strong>of</strong><br />

a circle or an ellipse. A satellite in a circular orbit travels<br />

at a constant speed. <strong>The</strong> higher the altitude, however, the<br />

lower the speed relative <strong>to</strong> the surface <strong>of</strong> the Earth. Main-<br />

taining an altitude <strong>of</strong> 35,800 km over the equa<strong>to</strong>r, a satellite<br />

is said <strong>to</strong> be in geostationary orbit. In an elliptical<br />

orbit, the speed varies and is greatest at perigee (minimum<br />

altitude) and least at apogee (maximum altitude).<br />

Elliptical orbits can lie in any plane that passes through<br />

Earth’s center. A polar orbit lies in a plane that passes<br />

through the North and South Poles; in other words, it<br />

passes through Earth’s axis <strong>of</strong> rotation. An equa<strong>to</strong>rial<br />

orbit is one that lies in a plane passing through the equa<strong>to</strong>r.<br />

<strong>The</strong> angle between the orbital plane and the equa<strong>to</strong>rial<br />

plane is called the inclination <strong>of</strong> the orbit. As long as<br />

the orbit <strong>of</strong> an object keeps it in the vacuum <strong>of</strong> space, the<br />

object will continue <strong>to</strong> orbit without propulsive power<br />

because there is no frictional force <strong>to</strong> slow it down. If part<br />

or all <strong>of</strong> the orbit passes through Earth’s atmosphere,<br />

however, the body is slowed by aerodynamic friction<br />

with the air. This causes the orbit <strong>to</strong> decay gradually <strong>to</strong><br />

lower and lower altitudes until the object fully reenters<br />

the atmosphere and burns up. An open orbit is one in<br />

which a spacecraft does not follow a closed circuit<br />

around a gravitating body but simply has its path bent<br />

in<strong>to</strong> the shape <strong>of</strong> a parabola or a hyperbola. 210<br />

orbit decay<br />

A gradual change in the orbit <strong>of</strong> a spacecraft caused by<br />

the aerodynamic drag <strong>of</strong> a planet’s outer atmosphere and<br />

other forces. <strong>The</strong> rate <strong>of</strong> orbit decay rises as the spacecraft<br />

falls and encounters increasing atmospheric density,<br />

eventually resulting in reentry.<br />

orbital curve<br />

<strong>The</strong> trace <strong>of</strong> an orbit on a flattened map <strong>of</strong> Earth or<br />

another celestial body about which the spacecraft is orbiting.<br />

Each successive orbit is displaced by the amount <strong>of</strong><br />

rotation <strong>of</strong> the body between each orbit.<br />

orbital cycler<br />

An economical method <strong>of</strong> travel within the Solar System<br />

proposed by Buzz Aldrin. It turns out that there are stable<br />

orbits that cross the orbits <strong>of</strong> both Earth and Mars.<br />

Aldrin has suggested placing a large permanent station in<br />

such an orbit. Travelers would embark on the station<br />

when it passed Earth and disembark as it passed Mars.<br />

<strong>The</strong> energy cost for the traveler is simply the cost <strong>to</strong> make<br />

the rendezvous at each end.<br />

orbital elements<br />

Six quantities that are used <strong>to</strong> describe the motion <strong>of</strong> an<br />

orbiting object, such as that <strong>of</strong> a satellite around the<br />

Earth. <strong>The</strong>y are: (1) the semi-major axis, which defines<br />

the size <strong>of</strong> the orbit; (2) the eccentricity, which defines<br />

the shape <strong>of</strong> the orbit; (3) the inclination, which (in the

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