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
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460 Vanguard<br />
fired from here in December 1958. Since then, Vandenberg<br />
has acquired pads and support facilities for launching<br />
other rockets, including versions <strong>of</strong> the Atlas, Delta,<br />
Titan, and Scout. Because <strong>of</strong> its location, with open water<br />
<strong>to</strong> the south, it is America’s premier launch site for polar<br />
missions. It was also originally intended <strong>to</strong> serve as a<br />
launch center for polar Space Shuttle missions, and construction<br />
<strong>of</strong> Shuttle launch facilities at VAFB was begun.<br />
However, this was permanently halted after the Challenger<br />
disaster and the decision <strong>of</strong> the Department <strong>of</strong><br />
Defense <strong>to</strong> use expendable launch vehicles for highpriority<br />
polar military payloads.<br />
Vanguard<br />
See article, pages 461–462.<br />
VASIMR (Variable Specific Impulse<br />
Magne<strong>to</strong>plasma Rocket)<br />
A plasma engine that has been under development by a<br />
NASA astronaut for the past two decades. Astronaut<br />
Franklin Chang-Diaz began work on the rocket technology<br />
in 1979, when he was a graduate student at the Massachusetts<br />
Institute <strong>of</strong> Technology. Since late 1993,<br />
Chang-Diaz and colleagues have continued work on the<br />
engine at the Advanced Space Propulsion Labora<strong>to</strong>ry at<br />
the Johnson Space Center. Unlike conventional rocket<br />
engines, which ignite a mix <strong>of</strong> fuel and oxidizer <strong>to</strong> generate<br />
thrust, VASIMR uses a series <strong>of</strong> magnetic fields <strong>to</strong> create<br />
and accelerate plasma, or high-temperature ionized<br />
gas. <strong>The</strong> process begins when neutral hydrogen gas is<br />
injected in<strong>to</strong> the first <strong>of</strong> three magnetic cells. That cell<br />
ionizes the gas, stripping away the sole electron from<br />
each hydrogen a<strong>to</strong>m. <strong>The</strong> gas then moves in<strong>to</strong> the central<br />
magnetic cell, where radio waves, generated in a manner<br />
similar <strong>to</strong> a microwave oven, heat the gas <strong>to</strong> more than<br />
50,000°C, turning it in<strong>to</strong> a high-temperature plasma. <strong>The</strong><br />
plasma is then injected in<strong>to</strong> the last magnetic cell, a magnetic<br />
nozzle, which directs the plasma in<strong>to</strong> an exhaust<br />
that provides thrust for the engine. A key advantage <strong>of</strong><br />
the engine is that its specific impulse—a measure <strong>of</strong> the<br />
velocity <strong>of</strong> its exhaust—can be varied in flight <strong>to</strong> change<br />
the amount <strong>of</strong> thrust. <strong>The</strong> specific impulse <strong>of</strong> the engine<br />
can be turned down <strong>to</strong> provide additional thrust during<br />
key portions <strong>of</strong> a mission, then turned up during cruise<br />
phases <strong>to</strong> improve efficiency. If VASIMR is successfully<br />
developed, it could cut in half the time needed for travel<br />
<strong>to</strong> Mars. By firing continuously, accelerating during the<br />
first half <strong>of</strong> the flight, and then turning <strong>to</strong> deaccelerate<br />
the spacecraft for the second half, VASIMR could send a<br />
human spacecraft <strong>to</strong> Mars in just over three months. In<br />
addition, VASIMR would enable such a mission <strong>to</strong> abort<br />
<strong>to</strong> Earth if problems developed during the early phases, a<br />
capability not available <strong>to</strong> conventional engines. A scale<br />
version <strong>of</strong> the VASIMR engine could fly in space as early<br />
as 2004 as part <strong>of</strong> the Radiation and Technology Demonstra<strong>to</strong>r<br />
spacecraft.<br />
VCL (Vegetation Canopy Lidar)<br />
A spacecraft that will use a radarlike imaging technique<br />
called lidar (light detection and ranging) <strong>to</strong> map the<br />
height <strong>of</strong> the world’s forests <strong>to</strong> an accuracy <strong>of</strong> one meter.<br />
VCL will shine five laser beams on<strong>to</strong> the forest’s canopy.<br />
By reconstructing the reflected light, the satellite will produce<br />
an accurate map <strong>of</strong> both the heights <strong>of</strong> the trees and<br />
the <strong>to</strong>pography <strong>of</strong> the underlying terrain. <strong>The</strong> data will<br />
be used <strong>to</strong> calculate the density and mass <strong>of</strong> the world’s<br />
vegetation, enabling scientists <strong>to</strong> moni<strong>to</strong>r the capacity <strong>of</strong><br />
forests <strong>to</strong> absorb carbon dioxide. In addition, the satellite<br />
will provide the first accurate estimate <strong>of</strong> how much carbon<br />
is being released in<strong>to</strong> Earth’s atmosphere through<br />
the burning <strong>of</strong> tropical rainforests. VCL is a mission <strong>of</strong><br />
NASA’s ESSP (Earth System Science Pathfinder) program;<br />
a launch date has yet <strong>to</strong> be decided.<br />
vec<strong>to</strong>r<br />
A quantity having both magnitude and direction; examples<br />
include velocity, acceleration, and force. Vec<strong>to</strong>rs<br />
are added when, for instance, movement takes place in a<br />
frame <strong>of</strong> reference that is itself moving (for example, as<br />
when a swimmer tries <strong>to</strong> cross a flowing river). Vec<strong>to</strong>rs are<br />
added like arrows, end <strong>to</strong> end, so that in the case <strong>of</strong> two<br />
vec<strong>to</strong>rs, the sum is the vec<strong>to</strong>r from the tail <strong>of</strong> the first <strong>to</strong><br />
the tip <strong>of</strong> the second.<br />
vec<strong>to</strong>r thrust<br />
A steering method in which one or more combustion<br />
chambers are mounted on gimbals so that the direction<br />
<strong>of</strong> the thrust force (thrust vec<strong>to</strong>r) may be tilted in relation<br />
<strong>to</strong> the center <strong>of</strong> gravity <strong>of</strong> the missile <strong>to</strong> produce turning.<br />
Vega 1 and 2<br />
Two identical Soviet spacecraft, each carrying a Venus<br />
lander and a Halley’s Comet flyby probe. <strong>The</strong> spacecraft<br />
released balloons in<strong>to</strong> the atmosphere <strong>of</strong> Venus and landers<br />
on<strong>to</strong> the surface before flying on <strong>to</strong> a rendezvous<br />
with Halley in March 1986. <strong>The</strong> twin Vegas passed 8,900<br />
km and 8,000 km, respectively, from the comet’s nucleus,<br />
returning pho<strong>to</strong>graphs and analyzing ejected gas and<br />
dust. (See table, “Vega Missions,” on page 463.)<br />
Launch vehicle: Pro<strong>to</strong>n<br />
Mass: 4,000 kg