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

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230 Lagrangian orbit<br />

carries an array <strong>of</strong> 426 prisms that reflect ground-based<br />

laser beams back <strong>to</strong> their source. By measuring the time<br />

between the transmission <strong>of</strong> the beam and the reception <strong>of</strong><br />

the reflected signal, stations can measure the distance<br />

between themselves and the satellite <strong>to</strong> an accuracy <strong>of</strong> 1 <strong>to</strong><br />

3 cm. Long-term data sets can be used <strong>to</strong> moni<strong>to</strong>r the<br />

motion <strong>of</strong> Earth’s tec<strong>to</strong>nic plates, measure Earth’s gravitational<br />

field, measure the wobble in Earth’s rotational axis,<br />

and better determine the length <strong>of</strong> an Earth day. Lageos 1<br />

was developed by NASA and placed in<strong>to</strong> a high inclination<br />

orbit <strong>to</strong> permit viewing by ground stations around the<br />

world. Lageos 2 was a joint program between NASA and<br />

ASI (the Italian Space Agency), which built the satellite<br />

using Lageos 1 specifications and materials provided by<br />

NASA. Lageos 2’s orbit was chosen <strong>to</strong> provide more coverage<br />

<strong>of</strong> seismically active areas, such as the Mediterranean<br />

Sea and California, and <strong>to</strong> help scientists understand irregularities<br />

noted in the motion <strong>of</strong> Lageos 1. Lageos 1 contains<br />

a message plaque addressed <strong>to</strong> humans and other<br />

beings <strong>of</strong> the far future with maps <strong>of</strong> Earth from three different<br />

eras—268 million years in the past, the present day,<br />

and 8 million years in the future (the satellite’s estimated<br />

decay date). Both satellites are spherical bodies with an aluminum<br />

shell wrapped around a brass core. <strong>The</strong> design was<br />

a compromise between numerous fac<strong>to</strong>rs, including the<br />

need <strong>to</strong> be as heavy as possible <strong>to</strong> minimize the effects <strong>of</strong><br />

nongravitational forces, <strong>to</strong> be light enough <strong>to</strong> be placed in<br />

a high orbit, <strong>to</strong> accommodate as many retroreflec<strong>to</strong>rs as<br />

possible, and <strong>to</strong> minimize surface area <strong>to</strong> minimize the<br />

effects <strong>of</strong> solar pressure. <strong>The</strong> materials were chosen <strong>to</strong><br />

reduce the effects <strong>of</strong> Earth’s magnetic field on the satellite’s<br />

orbit. (See table, “Lageos Missions.”)<br />

Lagrangian orbit<br />

<strong>The</strong> orbit <strong>of</strong> an object located at one <strong>of</strong> the Lagrangian<br />

points.<br />

Lagrangian point<br />

One <strong>of</strong> five equilibrium points at which a spacecraft or<br />

some other small object can remain in the same relative<br />

position in the orbital plane <strong>of</strong> two massive bodies, such as<br />

the Earth and the Sun, or the Earth and the Moon.<br />

Lagrangian points are named after the Italian-born French<br />

mathematician Joseph Louis de Lagrange (1736–1813),<br />

Lageos Missions<br />

who first demonstrated their existence mathematically. Two<br />

<strong>of</strong> these points, known as L4 and L5, are said <strong>to</strong> be stable<br />

because an object placed at one <strong>of</strong> them will, if slightly displaced,<br />

return <strong>to</strong> the point rather than move farther away.<br />

<strong>The</strong> L5 point <strong>of</strong> the Earth-Moon system, located 60°<br />

behind the Moon in its orbit (as seen from Earth), has been<br />

proposed as an ideal site for a space colony. However, <strong>to</strong><br />

date, all practical spaceflight applications have focused on<br />

unstable Lagrangian points—L1, L2, and L3—so called<br />

because the slightest disturbance <strong>to</strong> any object located at<br />

one <strong>of</strong> them will cause the object <strong>to</strong> drift away permanently<br />

unless it makes a correction (a station-keeping maneuver)<br />

using an onboard propulsion system. <strong>The</strong> L1 and L2 points<br />

have proven particularly useful and are being used increasingly<br />

by a variety <strong>of</strong> scientific satellites. <strong>The</strong> L1 point <strong>of</strong> the<br />

Sun-Earth system—about 1.5 million km directly Sunward<br />

<strong>of</strong> Earth—affords a good spot for moni<strong>to</strong>ring the solar wind,<br />

which reaches it about one hour before reaching Earth.<br />

Beginning in 1978, ISEE-3 carried out solar wind observations<br />

from the L1 region for several years. More recently,<br />

Wind, SOHO, ACE, and Genesis have studied the Sun<br />

and its particle emissions from the same celestial perch. <strong>The</strong><br />

preferred position is actually some distance <strong>to</strong> the side <strong>of</strong><br />

L1, for if the spacecraft is right on the Sun-Earth line, the<br />

antennas that track it from Earth are also aimed at the Sun,<br />

which is an intense source <strong>of</strong> interfering radio waves. At the<br />

Spacecraft Date<br />

Launch<br />

Vehicle Site Orbit Mass (kg)<br />

Lageos 1 May 4, 1976 Delta 2914 Vandenberg 5,837 × 5,945 km × 109.8° 411<br />

Lageos 2 Oct. 22, 1992 Shuttle STS-52 Cape Canaveral 5,615 × 5,952 km × 52.6° 400<br />

L3<br />

Sun<br />

L4<br />

L5<br />

L1 L2<br />

Earth<br />

Lagrangian point <strong>The</strong> five Lagrangian points in the Sun-<br />

Earth system.

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