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

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the intended geosynchronous one, its mission was ultimately<br />

a triumph and resulted in two catalogues: the<br />

Hipparcos catalogue <strong>of</strong> 118,000 stars with positions, parallaxes,<br />

and proper motions measured <strong>to</strong> an unprecedented<br />

accuracy <strong>of</strong> 2 milliarcseconds (see arcseconds),<br />

and the Tycho catalogue <strong>of</strong> over a million stars with measurements<br />

<strong>of</strong> somewhat lower accuracy. Its mission ended<br />

in 1993 and its final catalogue was published in 1997.<br />

Launch<br />

Date: August 8, 1989<br />

Vehicle: Ariane 44<br />

Site: Kourou<br />

Orbit: 542 × 35,836 km × 6.7°<br />

Mass: 1,130 kg<br />

Hiten<br />

A Japanese lunar probe, launched by ISAS (Institute <strong>of</strong><br />

Space and Astronautical Science), that made multiple flybys<br />

<strong>of</strong> the Moon from an extremely elliptical Earth orbit<br />

and released Hagoromo, a smaller satellite, in<strong>to</strong> lunar<br />

orbit. Hiten itself was put in<strong>to</strong> lunar orbit in February<br />

1992 and crashed in<strong>to</strong> the Moon on April 10, 1993. It<br />

was the first lunar probe not launched by the United<br />

States or Russia. Hiten, whose name means “celestial<br />

maiden,” was known before launch as MUSES-A.<br />

Launch<br />

Date: January 24, 1990<br />

Vehicle: M-3S<br />

Site: Kagoshima<br />

Orbit: 262 × 286,183 km × 30.6°<br />

Mass: 185 kg<br />

HNX (Heavy Nuclei Explorer)<br />

A space labora<strong>to</strong>ry for determining the properties <strong>of</strong> cosmic<br />

rays. HNX would directly sample and measure the<br />

properties <strong>of</strong> these high-speed suba<strong>to</strong>mic particles using<br />

silicon and glass detec<strong>to</strong>rs. It would be launched by the<br />

Space Shuttle and be retrieved three years later. HNX has<br />

been selected by NASA for study as a possible SMEX<br />

(Small Explorer) mission.<br />

Hohmann orbit<br />

An elliptical trajec<strong>to</strong>ry, named after Walter Hohmann,<br />

along which a spacecraft may move from one orbit <strong>to</strong><br />

another with the minimum expenditure <strong>of</strong> energy. Such<br />

an orbit just <strong>to</strong>uches the original and destination orbits,<br />

and may be used for changing the orbit <strong>of</strong> an Earth satellite<br />

or for sending a probe <strong>to</strong> another planet. It involves<br />

two firings <strong>of</strong> the spacecraft’s engine: one <strong>to</strong> break out <strong>of</strong><br />

the original orbit and another <strong>to</strong> enter the destination<br />

Hoover, George W. 185<br />

orbit. Its chief disadvantage is that it requires relatively<br />

long flight times. This can be overcome by judicious use<br />

<strong>of</strong> gravity-assists.<br />

Hohmann, Walter (1880–1945)<br />

A German rocket engineer who was a prominent member<br />

<strong>of</strong> the Verein für Raumschiffahrt (Society for Space<br />

Travel) in the late 1920s. His book, Die Erreichbarkeit der<br />

Himmelskörper (<strong>The</strong> Attainability <strong>of</strong> Celestial Bodies),<br />

published in 1925, was so technically advanced that it<br />

was consulted decades later by NASA when planning its<br />

first interplanetary probes. In it, he describes his “power<br />

<strong>to</strong>wer” spacecraft, a huge cone-shaped rocket with an eggshaped<br />

manned capsule at the <strong>to</strong>p, and, more important,<br />

the interplanetary transfer orbits that have been named<br />

after him (see Hohmann orbit). He also wrote popular<br />

works in the field <strong>of</strong> rocketry, as did his contemporaries<br />

Willy Ley and Max Valier.<br />

hold<br />

A scheduled pause or unscheduled delay in the launching<br />

sequence or countdown <strong>of</strong> a space vehicle or missile.<br />

hold-down test<br />

<strong>The</strong> testing <strong>of</strong> a system or subsystem in a launch vehicle<br />

while the vehicle is restrained in a stand.<br />

holding fixture<br />

A device or equipment used <strong>to</strong> support and position the<br />

upper launch vehicle stages and the spacecraft modules<br />

during test, checkout, and handling operations.<br />

holding pond<br />

Also known as a skimming basin, a human-made basin<br />

in<strong>to</strong> which spilled propellants, deluge water, and washdown<br />

water are drained from the launch pad, launcher<br />

area, and launcher platform. <strong>The</strong> pond is so constructed<br />

that the water can be drained and the propellants<br />

skimmed for disposal.<br />

Hoover, George W.<br />

An early advocate <strong>of</strong> American satellite launches and an<br />

instiga<strong>to</strong>r <strong>of</strong> Project Orbiter. Hoover entered the Navy in<br />

1944 and became a pilot before moving <strong>to</strong> the Office <strong>of</strong><br />

Naval Research <strong>to</strong> conduct a program in all-weather flight<br />

instrumentation. Later he helped develop the idea <strong>of</strong><br />

high-altitude balloons for use in a variety <strong>of</strong> projects.<br />

<strong>The</strong>se included Skyhook, which supported cosmic-ray<br />

research and served as a research vehicle for obtaining<br />

environmental data relevant <strong>to</strong> supersonic flight. In<br />

1954, Hoover was project <strong>of</strong>ficer in the field <strong>of</strong> highspeed,<br />

high-altitude flight, with involvement in the<br />

Douglas D558 project leading <strong>to</strong> the X-15. He was also

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