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

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140 flux<br />

it also supported AFSATCOM (Air Force Satellite Communications<br />

System), which is a vital component <strong>of</strong> the<br />

American strategic nuclear capability.<br />

flux<br />

A measure <strong>of</strong> the energy or number <strong>of</strong> particles passing<br />

through a given area <strong>of</strong> a surface in unit time. Luminous<br />

flux is the rate <strong>of</strong> flow <strong>of</strong> energy in the form <strong>of</strong> pho<strong>to</strong>ns.<br />

Particle flux is the number <strong>of</strong> particles (for example, in the<br />

solar wind) passing through a unit area per second. Magnetic<br />

flux is a measure <strong>of</strong> the strength <strong>of</strong> a magnetic field<br />

perpendicular <strong>to</strong> a surface.<br />

flux density<br />

<strong>The</strong> energy in a beam <strong>of</strong> radiation passing through a unit<br />

area at right angles <strong>to</strong> the beam per unit time.<br />

fly-away disconnects<br />

Umbilical or other connections <strong>to</strong> the various stages <strong>of</strong> a<br />

space vehicle that disconnect from the vehicle at lift<strong>of</strong>f,<br />

either mechanically or by the actual rising <strong>of</strong> the vehicle<br />

<strong>of</strong>f the launch pad.<br />

flyby<br />

A type <strong>of</strong> space mission in which the spacecraft passes<br />

close <strong>to</strong> its target but does not enter orbit around it or<br />

land on it.<br />

flyby maneuver<br />

See gravity-assist.<br />

Fobos<br />

Two nearly identical Soviet spacecraft intended <strong>to</strong><br />

explore Mars from orbit and land probes on Phobos, the<br />

larger (but still very small) Martian moon. One failed<br />

completely, the other partially. <strong>The</strong> mission involved<br />

cooperation with 14 other nations including Sweden,<br />

Switzerland, Austria, France, West Germany, and the<br />

United States (which contributed the use <strong>of</strong> its Deep<br />

Space Network for tracking). As well as onboard instruments,<br />

each vehicle carried a lander designed <strong>to</strong> carry<br />

out various measurements on Phobos’s surface. Phobos<br />

2 also carried a second, smaller “hopper” lander<br />

designed <strong>to</strong> move about using spring-loaded legs and<br />

make chemical, magnetic, and gravimetric observations<br />

at different locations. Phobos 2 operated according <strong>to</strong><br />

plan throughout its cruise and Mars orbital-insertion<br />

phases, gathering data on the Sun, interplanetary medium,<br />

Mars, and Phobos. However, contact with the<br />

probe was lost on March 27, 1989, two months after it<br />

had entered Martian orbit and shortly before the final<br />

phase <strong>of</strong> the mission during which the spacecraft was <strong>to</strong><br />

approach within 50 m <strong>of</strong> Phobos’s surface and release its<br />

landers. <strong>The</strong> cause <strong>of</strong> the failure was found <strong>to</strong> be a malfunction<br />

<strong>of</strong> the onboard computer. Contact with Phobos<br />

1 had been lost much earlier, while the spacecraft<br />

was en route <strong>to</strong> Mars. This failure was traced <strong>to</strong> an error<br />

in the s<strong>of</strong>tware uploaded <strong>to</strong> the probe, which had deactivated<br />

its attitude thrusters. This caused a loss <strong>of</strong> lock on<br />

the Sun, resulting in the spacecraft orienting its solar<br />

arrays away from the Sun, thus depleting the batteries. It<br />

remains in solar orbit.<br />

Launch<br />

Date: July 7, 1988 (Fobos 1); July 12, 1988 (Fobos 2)<br />

Vehicle: Pro<strong>to</strong>n<br />

Site: Baikonur<br />

Mass (at Mars): 2,600 kg<br />

FOBS (Fractional Orbital Bombardment System)<br />

An orbital variant <strong>of</strong> the Soviet R-36 intercontinental ballistic<br />

missile, known in Russia as the R-360 (see “R”<br />

series <strong>of</strong> Russian missiles) and intended <strong>to</strong> deliver<br />

nuclear warheads from space. <strong>The</strong> Western designation<br />

“FOBS” refers <strong>to</strong> the fact that although the payloads<br />

reached orbit, they were intended <strong>to</strong> reenter over their<br />

targets prior <strong>to</strong> completing a full circuit <strong>of</strong> the Earth.<br />

Four suborbital FOBS tests were carried out between<br />

December 1965 and May 1966. <strong>The</strong>se were followed by<br />

more tests through 1971, delivering 5-<strong>to</strong>n payloads in<strong>to</strong><br />

low Earth orbit. FOBS is a direct ances<strong>to</strong>r <strong>of</strong> the modernday<br />

commercial Tsyklon launch vehicle.<br />

Fontana, Giovanni da (c. 1395–1455)<br />

An Italian author <strong>of</strong> a sketchbook, Bellicorum instrumen<strong>to</strong>rum<br />

liber (<strong>Book</strong> <strong>of</strong> War Instruments), published in 1420,<br />

in which appear various rocket-propelled devices including<br />

a cart designed <strong>to</strong> smash through enemy strongholds<br />

and a surface-running <strong>to</strong>rpedo for setting fire <strong>to</strong> enemy<br />

ships.<br />

footprint<br />

(1) In the case <strong>of</strong> a communications satellite, a map <strong>of</strong><br />

the signal strength showing the power con<strong>to</strong>urs <strong>of</strong> equal<br />

signal strengths as they cover the Earth’s surface. (2) In<br />

the case <strong>of</strong> a spacecraft lander, the area within which the<br />

vehicle is targeted <strong>to</strong> <strong>to</strong>uch down.<br />

force<br />

In mechanics, the cause <strong>of</strong> a change in motion <strong>of</strong> an<br />

object. It is measured by the rate <strong>of</strong> change <strong>of</strong> the object’s<br />

momentum.

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