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

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HEO<br />

(1) Highly elliptical orbit. Definitions vary, one being an<br />

orbit with a perigee (low point) below 3,000 km and an<br />

apogee (high point) above 30,000 km. (2) High Earth<br />

orbit. An orbit whose apogee lies above that <strong>of</strong> a geostationary<br />

orbit at 35,800 km.<br />

HEOS (Highly Eccentric Orbiting Satellite)<br />

ESRO (European Space Research Organisation) satellites<br />

that traveled in extremely elongated orbits in order <strong>to</strong><br />

study the interplanetary magnetic field outside Earth’s<br />

magne<strong>to</strong>sphere. (See table, “HEOS Missions.”)<br />

Hermes<br />

A proposed small, manned space plane for servicing<br />

European components <strong>of</strong> the International Space Station.<br />

It began as a purely French project, but as development<br />

costs increased, France managed <strong>to</strong> obtain other<br />

European funding, primarily from Germany, for development<br />

<strong>of</strong> the craft. Hermes would have provided independent<br />

European manned access <strong>to</strong> space, and the<br />

weight growth <strong>of</strong> the spacecraft during design and development<br />

was a major influence in the specification for the<br />

Ariane 5 launcher. Hermes was intended <strong>to</strong> take three<br />

astronauts <strong>to</strong> orbits <strong>of</strong> up <strong>to</strong> 800-km altitude on missions<br />

lasting 30 <strong>to</strong> 90 days. Payload <strong>to</strong> be returned <strong>to</strong> Earth<br />

could be contained in a small payload bay, but most<br />

experiments were <strong>to</strong> be carried in an expendable pressurized<br />

supply module equipped with a docking port and<br />

mounted <strong>to</strong> the base <strong>of</strong> the glider. After the Challenger<br />

disaster, many safety features were added <strong>to</strong> Hermes,<br />

leading <strong>to</strong> further increases in weight and cost. In an<br />

emergency the crew cab could have been separated from<br />

the remainder <strong>of</strong> the glider. Later, however, the crew<br />

escape capsule idea was abandoned and was replaced by<br />

three ejection seats <strong>to</strong> save weight. Hermes was <strong>to</strong> have<br />

been launched a<strong>to</strong>p an Ariane 5 by 1998, but by 1992,<br />

estimated development costs rose <strong>to</strong> DM 12 billion and<br />

the project was abandoned.<br />

Hero <strong>of</strong> Alexandria (A.D. 1st century)<br />

Greek inven<strong>to</strong>r <strong>of</strong> the rocketlike device called an aeolipile.<br />

He lived about three centuries after another ancient<br />

rocketeer, Archytas.<br />

HEOS Missions<br />

HETE (High Energy Transient Experiment) 183<br />

Herschel Space Observa<strong>to</strong>ry<br />

A giant ESA (European Space Agency) space telescope<br />

with a 3.5-m-diameter main mirror (by comparison, Hubble’s<br />

is only 2.4 m across) designed <strong>to</strong> observe the universe<br />

in unprecedented detail at far infrared and<br />

submillimeter wavelengths from 80 <strong>to</strong> 670 microns and<br />

<strong>to</strong> carry out sensitive pho<strong>to</strong>metry and spectroscopy. Herschel<br />

will be launched <strong>to</strong>gether with Planck in early 2007<br />

by an Ariane 5. Once in space, the two satellites will separate<br />

and proceed <strong>to</strong> different orbits around the L2<br />

Lagrangian point, some 1.5 million km from Earth. Herschel,<br />

named after the great Hanoverian-born British<br />

astronomer William Herschel (1738–1822), was previously<br />

known as FIRST (Far Infrared and Submillimetre<br />

Space Telescope).<br />

HESSI (High Energy Solar Spectroscopic Imager)<br />

See RHESSI.<br />

HETE (High Energy Transient Experiment)<br />

A satellite whose main task is a multiwavelength study <strong>of</strong><br />

gamma-ray bursts using ultraviolet, X-ray, and gamma-ray<br />

instruments. A unique feature <strong>of</strong> the mission is its ability<br />

<strong>to</strong> localize bursts with an accuracy <strong>of</strong> several arcseconds<br />

in near real-time. <strong>The</strong>se positions are transmitted <strong>to</strong> the<br />

ground and picked up by a global network <strong>of</strong> primary<br />

and secondary ground stations, enabling rapid follow-up<br />

studies. <strong>The</strong> original HETE was lost following its launch<br />

on November 4, 1996, when it (and its co-passenger,<br />

SAC-B) failed <strong>to</strong> separate from the third stage <strong>of</strong> a Pegasus<br />

launch vehicle. However, the scientific importance<br />

and continuing relevance <strong>of</strong> the mission provided the<br />

impetus for the mission collabora<strong>to</strong>rs, including NASA,<br />

CESR (Centre d’Etude Spatiale des Rayonnements),<br />

CNES (the French space agency), and RIKEN (Japan’s<br />

Institute <strong>of</strong> Chemical and Physical Research), <strong>to</strong> fund a<br />

replacement satellite. HETE-2 retains nearly all the original<br />

HETE design elements but carries a s<strong>of</strong>t (longer wavelength)<br />

X-ray camera in place <strong>of</strong> the original ultraviolet<br />

cameras. Its main instrument is FREGATE, the French<br />

Gamma Telescope, a hard (shorter wavelength) X-ray<br />

spectrometer operating in the 6 <strong>to</strong> 400 keV energy range.<br />

This gamma-ray burst detec<strong>to</strong>r, <strong>to</strong>gether with a Wide<br />

Field X-ray Moni<strong>to</strong>r, is used <strong>to</strong> trigger searches with the<br />

Spacecraft Date<br />

Launch<br />

Vehicle Site Orbit Mass (kg)<br />

HEOS 1 Dec. 5, 1968 Delta E Cape Canaveral 20,020 × 202,780 km × 60.5° 108<br />

HEOS 2 Jan. 31, 1972 Delta L Vandenberg 405 × 240,164 km × 89.9° 123

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