13.12.2012 Views

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

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Solar-B<br />

A Japan-led mission, with collaboration from the United<br />

States and Britain, <strong>to</strong> follow-on from the highly successful<br />

Yohkoh (Solar-A). It will look at the Sun in s<strong>of</strong>t<br />

(longer wavelength) X-rays, as does Yohkoh, but will also<br />

provide very high-resolution images in visible light.<br />

Solar-B will carry a coordinated set <strong>of</strong> optical, extreme<br />

ultraviolet, and X-ray instruments <strong>to</strong> investigate the interaction<br />

between the Sun’s magnetic field and its corona.<br />

<strong>The</strong> result will be an improved understanding <strong>of</strong> the<br />

mechanisms that underlie solar magnetic variability and<br />

how this variability affects the <strong>to</strong>tal solar output. ISAS<br />

(Institute <strong>of</strong> Space and Astronautical Science) will provide<br />

the spacecraft, the M-5 launch vehicle, and major<br />

elements <strong>of</strong> each <strong>of</strong> the scientific instruments. <strong>The</strong>se<br />

include a 0.5-m solar optical telescope (SOT), an X-ray<br />

telescope (XRT), and an extreme ultraviolet imaging<br />

spectrometer (EIS). Britain’s Particle Physics and Astronomical<br />

Research Council is responsible for the EIS.<br />

NASA will provide the focal plane package (FPP) for the<br />

SOT, as well as components <strong>of</strong> the XRT and EIS. Solar-B<br />

is scheduled for launch in the fall <strong>of</strong> 2005 in<strong>to</strong> a sunsynchronous<br />

orbit that will keep the instruments in<br />

nearly continuous sunlight.<br />

solar-electric propulsion (SEP)<br />

A form <strong>of</strong> electric propulsion in which the electrical<br />

energy used <strong>to</strong> accelerate the propellant comes from a<br />

solar power source, such as arrays <strong>of</strong> pho<strong>to</strong>voltaic cells.<br />

solid propellant<br />

A rocket propellant in solid form, usually containing<br />

both fuel and oxidizer combined, or mixed and formed,<br />

in<strong>to</strong> a monolithic (not powdered or granulated) grain.<br />

Solid Rocket Boosters (SRBs)<br />

See Space Shuttle.<br />

solid-fueled rockets<br />

Rockets that burn a solid mixture <strong>of</strong> fuel and oxidizer and<br />

that have no separation between combustion chamber<br />

and fuel reservoir. Gunpowder is such a mixture and was<br />

the earliest rocket fuel. <strong>The</strong>y are somewhat less efficient<br />

than the best liquid-fueled rockets, but they are preferred<br />

for military use because they need no lengthy preparation<br />

and are easily s<strong>to</strong>red in ready-<strong>to</strong>-fly condition. <strong>The</strong>y<br />

are also used in auxiliary rockets that help heavily loaded<br />

liquid-fueled rockets, such as the Space Shuttle and Delta<br />

rockets, lift <strong>of</strong>f and go through the first stage <strong>of</strong> their flight.<br />

solid-propellant rocket mo<strong>to</strong>r<br />

A rocket propulsion system in which the propellantis contained<br />

within the combustion chamberor case. <strong>The</strong> solid<br />

Solwind 385<br />

propellant charge is called the grain and contains all the<br />

chemical constituents for complete burning. Once ignited,<br />

it usually burns smoothly at a predetermined rate on all<br />

the exposed surfaces <strong>of</strong> the grain. <strong>The</strong> internal cavity grows<br />

as propellant is burned and consumed. <strong>The</strong> resulting hot<br />

gas flows through the supersonic nozzle <strong>to</strong> impart thrust.<br />

Once ignited, the combustion proceeds until all the propellant<br />

is used up. <strong>The</strong>re are no feed systems or valves.<br />

SOLO (Solar Orbiter)<br />

A proposed ESA (European Space Agency) Sun-orbiting<br />

spacecraft that will carry optical instruments <strong>to</strong> view the<br />

Sun directly from close up and from high latitudes.<br />

SOLO will study fields and particles in the part <strong>of</strong> the<br />

heliosphere near <strong>to</strong> the Sun, the links between activity on<br />

the Sun’s surface and the corona, and the Sun’s polar<br />

regions. <strong>The</strong> spacecraft will tap much <strong>of</strong> the technology<br />

developed for Bepi Colombo, the Mercury Corners<strong>to</strong>ne<br />

mission. <strong>The</strong> orbital design follows the Mercury Orbiter<br />

trajec<strong>to</strong>ry design, and the mission will use solar-electric<br />

propulsion (SEP), powered by a set <strong>of</strong> large cruise solar<br />

arrays that are jettisoned after the last firing <strong>of</strong> the SEP<br />

thrusters. Using SEP <strong>to</strong>gether with multiple gravity-assist<br />

maneuvers, it will take Solar Orbiter only two years <strong>to</strong><br />

reach a perihelion <strong>of</strong> 45 solar radii at an orbital period <strong>of</strong><br />

149 days.<br />

Solrad (Solar Radiation program)<br />

A series <strong>of</strong> missions, conceived by the U.S. Naval<br />

Research Labora<strong>to</strong>ry in the late 1950s, <strong>to</strong> study the effects<br />

<strong>of</strong> solar emissions on the ionosphere and also <strong>to</strong> conceal<br />

the existence <strong>of</strong> classified intelligence satellites, known as<br />

GRAB, that were launched at the same time. <strong>The</strong> Solrad<br />

series was designed <strong>to</strong> provide continuous coverage <strong>of</strong><br />

wavelength and intensity changes <strong>of</strong> solar radiation in the<br />

ultraviolet, s<strong>of</strong>t (longer wavelength) X-ray, and hard<br />

(shorter wavelength) X-ray ranges. All missions up <strong>to</strong> Solrad<br />

7B were GRAB copassengers. Solrad 8, 9, and 10 were<br />

also known as Explorer 30, 37 (or Solar Explorer B), and<br />

44, respectively.<br />

Solwind<br />

A satellite designed <strong>to</strong> investigate how the solar wind<br />

interacts with Earth’s ionosphere and magne<strong>to</strong>sphere. It<br />

was destroyed, while still functional, on September 13,<br />

1985, as part <strong>of</strong> a U.S. Air Force antisatellite (ASAT) test.<br />

Launch<br />

Date: February 24, 1979<br />

Vehicle: Atlas F<br />

Site: Vandenberg Air Force Base<br />

Orbit: 310 × 317 km × 97.8°<br />

Mass: 1,331 kg

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!