The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
mass<br />
In general, the amount <strong>of</strong> matter in a body. Mass can be<br />
defined more precisely in terms <strong>of</strong> how difficult it is <strong>to</strong><br />
change a body’s state <strong>of</strong> motion or how great is the<br />
body’s gravitational effect on other objects. <strong>The</strong> first <strong>of</strong><br />
these is called inertial mass and is given by the fac<strong>to</strong>r m in<br />
New<strong>to</strong>n’s second law F = ma. <strong>The</strong> second is called gravitational<br />
mass and is the mass corresponding <strong>to</strong> an object’s<br />
weight in a local gravitational field—the m in F = mg for an<br />
object on or near the Earth. According <strong>to</strong> all experiments,<br />
the values for m arising from these two definitions<br />
are identical. Einstein’s mass-energy relationship also<br />
shows that mass and energy are interchangeable.<br />
mass driver<br />
An electromagnetic cannon that would be able <strong>to</strong> accelerate<br />
payloads from the surface <strong>of</strong> a low-gravity world,<br />
such as the Moon or an asteroid, in<strong>to</strong> space. 51<br />
mass ratio<br />
<strong>The</strong> ratio <strong>of</strong> the initial mass <strong>of</strong> a spacecraft, or one <strong>of</strong> its<br />
stages, <strong>to</strong> the final mass after consumption <strong>of</strong> the propellant.<br />
mass-energy relationship<br />
Einstein’s famous equation E = mc 2 . This shows that mass<br />
and energy are really two sides <strong>of</strong> the same coin. It also<br />
gives the amount <strong>of</strong> energy E that results when a mass m is<br />
completely turned in<strong>to</strong> energy, c being the speed <strong>of</strong> light.<br />
<strong>The</strong> fact that c squared is a huge number indicates that a<br />
vast amount <strong>of</strong> energy can come from even a tiny amount<br />
<strong>of</strong> matter. Mass-<strong>to</strong>-energy conversion is the basic principle<br />
at work in some advanced propulsion schemes such as the<br />
nuclear pulse rocket and antimatter propulsion.<br />
MASTIF (Multiple Axis Space Test Inertia Facility)<br />
A three-axis gimbal rig, built by the Lewis Research Center<br />
(now the Glenn Research Center), which simulated<br />
tumble-type maneuvers that might be encountered during<br />
a space mission. Three tubular aluminum cages could<br />
revolve separately or in combination <strong>to</strong> give roll, pitch,<br />
and yaw motions at speeds up <strong>to</strong> 30 rpm, greater than<br />
those expected in actual spaceflight. Nitrogen-gas jets<br />
attached <strong>to</strong> the three cages controlled the motion. At the<br />
center <strong>of</strong> the innermost cage, the pilot was strapped in<strong>to</strong><br />
a plastic seat similar <strong>to</strong> that in a Mercury capsule. His<br />
head, body, and legs were held in place, leaving only his<br />
arms free. <strong>The</strong> pilot actuated the jets by means <strong>of</strong> a righthand<br />
control column. Communication was by radio,<br />
which was operated by a but<strong>to</strong>n a<strong>to</strong>p the left-hand column.<br />
Complex tumbling motions were started by the<br />
opera<strong>to</strong>r at the control station, and control then switched<br />
Mattingly, Thomas K., II 267<br />
<strong>to</strong> the pilot. By reading instruments mounted at eye level<br />
before him, the pilot interpreted his motions and made<br />
corrections accordingly. <strong>From</strong> February 15 <strong>to</strong> March 4,<br />
1960, MASTIF provided training for all seven Project<br />
Mercury astronauts. Each experienced about five hours<br />
<strong>of</strong> “flight time.” Later that year, a set <strong>of</strong> woman pilots also<br />
used the device as part <strong>of</strong> a broader assessment <strong>of</strong> abilities<br />
(see Mercury Thirteen). In addition, the rig was used <strong>to</strong><br />
evaluate instrument control systems for spaceflight and<br />
<strong>to</strong> study the physiological effects <strong>of</strong> spinning, such as eye<br />
oscillation and motion sickness.<br />
Matador<br />
<strong>The</strong> first successful surface-<strong>to</strong>-surface, pilotless, tactical<br />
weapon developed for the U.S. Air Force. A highly<br />
mobile system designed <strong>to</strong> deliver a warhead on tactical<br />
missions in support <strong>of</strong> ground troops for a distance <strong>of</strong> up<br />
<strong>to</strong> 960 km, the Matador project began shortly after the<br />
end <strong>of</strong> World War II. Test firings began in 1949 in Alamogordo,<br />
New Mexico, and by January 1951 the Matador<br />
was in production.<br />
Matagorda Island<br />
Located 80 km northeast <strong>of</strong> Corpus Christi, Texas, at<br />
28.5° N, 96.5° W, the site <strong>of</strong> a private launch pad used by<br />
Space Services <strong>to</strong> launch its Cones<strong>to</strong>ga rocket in 1982.<br />
Mattingly, Thomas K., II (1936–)<br />
A veteran American astronaut involved in both the<br />
<strong>Apollo</strong> and Space Shuttle programs. Mattingly received<br />
a B.S. in aeronautical engineering from Auburn University<br />
in 1958 and subsequently flew carrier-based aircraft.<br />
Selected by NASA in April 1966, he served as a member<br />
<strong>of</strong> the astronaut support crews for the <strong>Apollo</strong> 8 and<br />
<strong>Apollo</strong> 11 missions, and he was also the astronaut representative<br />
in the development and testing <strong>of</strong> the <strong>Apollo</strong><br />
spacesuit and backpack. Although designated as the<br />
Command Module pilot for <strong>Apollo</strong> 13, he was removed<br />
from flight status 72 hours before the scheduled launch<br />
because <strong>of</strong> exposure <strong>to</strong> German measles. Mattingly subsequently<br />
served as Command Module pilot <strong>of</strong> <strong>Apollo</strong><br />
16 and head <strong>of</strong> astronaut <strong>of</strong>fice support <strong>to</strong> the Space<br />
Shuttle program from January 1973 <strong>to</strong> March 1978. He<br />
was next assigned as technical assistant for flight test <strong>to</strong><br />
the manager <strong>of</strong> the Orbital Flight Test Program. <strong>From</strong><br />
December 1979 <strong>to</strong> April 1981, he headed the Astronaut<br />
Office ascent/entry group. He subsequently served as<br />
backup commander for STS-2 and STS-3, Columbia’s second<br />
and third orbital test flights. Mattingly was commander<br />
for the fourth and final orbital test flights <strong>of</strong> the<br />
Shuttle Columbia (STS-4) on June 27, 1982, and was also<br />
commander for the first Department <strong>of</strong> Defense (DoD)