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

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22 antiparticle<br />

efficient space propulsion system that would need<br />

only a tiny fraction <strong>of</strong> the antimatter consumed by a<br />

beamed core engine. It would work by a process called<br />

antipro<strong>to</strong>n-catalyzed micr<strong>of</strong>ission (ACMF). 274 Whereas<br />

conventional nuclear fission can only transfer heat<br />

energy from a uranium core <strong>to</strong> surrounding chemical<br />

propellant, ACMF permits all energy from fission reactions<br />

<strong>to</strong> be used for propulsion. <strong>The</strong> result is a more efficient<br />

engine that could be used for interplanetary<br />

manned missions. <strong>The</strong> ICAN-II (Ion Compressed Antimatter<br />

Nuclear II) spacecraft designed at Penn State<br />

would use the ACMF engine and only 140 ng <strong>of</strong> antimatter<br />

for a manned 30-day crossing <strong>to</strong> Mars.<br />

A follow-up <strong>to</strong> ACMF and ICAN is a spacecraft propelled<br />

by AIM (antipro<strong>to</strong>n initiated micr<strong>of</strong>ission/fusion),<br />

in which a small concentration <strong>of</strong> antimatter and fissionable<br />

material would be used <strong>to</strong> spark a micr<strong>of</strong>usion reaction<br />

with nearby material. Using 30 <strong>to</strong> 130 micrograms <strong>of</strong><br />

antimatter, an unmanned AIM-powered probe—AIM-<br />

Star—would be able <strong>to</strong> travel <strong>to</strong> the Oort Cloud in 50<br />

years, while a greater supply <strong>of</strong> antipro<strong>to</strong>ns might bring<br />

Alpha Centauri within reach. 190<br />

antiparticle<br />

A counterpart <strong>of</strong> an ordinary suba<strong>to</strong>mic particle, which<br />

has the same mass and spin but opposite charge. Certain<br />

other properties are also reversed, including the<br />

magnetic moment. Antiparticles are the basis <strong>of</strong> antimatter.<br />

<strong>The</strong> antiparticles <strong>of</strong> the electron, pro<strong>to</strong>n, and<br />

neutron are the positron, antipro<strong>to</strong>n, and antineutron,<br />

respectively. An encounter between an electron and a<br />

positron results in the instantaneous <strong>to</strong>tal conversion<br />

<strong>of</strong> the mass <strong>of</strong> both in<strong>to</strong> energy in the form <strong>of</strong> gamma<br />

rays. When a pro<strong>to</strong>n and an antipro<strong>to</strong>n meet, however,<br />

the outcome is more complicated. Pions are produced,<br />

some <strong>of</strong> which decay <strong>to</strong> produce gamma radiation and<br />

others <strong>of</strong> which decay <strong>to</strong> produce muons and neutrinos<br />

plus electrons and positrons, which make more gamma<br />

rays.<br />

aphelion<br />

<strong>The</strong> point in a heliocentric orbit that is farthest from the<br />

Sun.<br />

apoapsis<br />

<strong>The</strong> point in an orbit that is farthest from the body being<br />

orbited. Special names, such as apogee and aphelion, are<br />

given <strong>to</strong> this point for familiar systems.<br />

apogee<br />

<strong>The</strong> point in a geocentric orbit that is farthest from Earth’s<br />

surface.<br />

apogee kick mo<strong>to</strong>r<br />

A solid rocket mo<strong>to</strong>r, usually permanently attached <strong>to</strong> a<br />

spacecraft, that circularizes an elliptical transfer orbit by<br />

igniting at apogee (leading <strong>to</strong> the colloquial phrase “a<br />

kick in the apogee”). It was first used on the early Syncom<br />

satellites in 1963 and 1964 <strong>to</strong> “kick” the satellite<br />

from a geostationary transfer orbit <strong>to</strong> a geostationary<br />

orbit. Also known simply as an apogee mo<strong>to</strong>r.<br />

<strong>Apollo</strong><br />

See article, pages 23–33.<br />

<strong>Apollo</strong>-Soyuz Test Project (ASTP)<br />

<strong>Apollo</strong> spacecraft<br />

Launch date: July 15, 1975<br />

Launch vehicle: Saturn IB<br />

Crew<br />

Commander: Thomas Stafford<br />

Command Module pilot: Vance Brand<br />

Docking Module pilot: Donald Slay<strong>to</strong>n<br />

Mission duration: 9 days 1 hr<br />

Splashdown: July 24, 1975<br />

Soyuz 19 spacecraft<br />

Crew<br />

Commander: Aleskei Leonov<br />

Flight engineer: Valeriy Kubasov<br />

Mission duration: 5 days 23 hr<br />

Landing: July 21, 1975<br />

<strong>The</strong> first international manned spaceflight and a symbolic<br />

end <strong>to</strong> the nearly 20-year-long Space Race between<br />

the United States and the Soviet Union. Setting political<br />

differences aside, the two superpowers successfully carried<br />

out the first joint on-orbit manned space mission.<br />

ASTP negotiations, begun in 1970, culminated in an<br />

agreement for ASTP flight operations being signed at the<br />

superpower summit in May 1972.<br />

<strong>The</strong> project was designed mainly <strong>to</strong> develop and validate<br />

space-based rescue techniques needed by both the<br />

American and the Soviet manned space programs. Science<br />

experiments would be conducted, and the logistics<br />

involved in carrying out joint space operations between<br />

the two nations would be tried and tested, paving the way<br />

for future joint ventures with the Space Shuttle, Mir, and<br />

the International Space Station (ISS). As the American<br />

and Soviet space capsules were incompatible, a new docking<br />

module had <strong>to</strong> be built with a Soviet port on one side<br />

and an American port on the other. This module also<br />

served as an airlock and a transfer facility, allowing astronauts<br />

and cosmonauts <strong>to</strong> acclimatize <strong>to</strong> the atmospheres<br />

(continued on page 34)

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