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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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186 HOPE (H-2 Orbital Plane)<br />

instrumental in establishing Project Orbiter with von<br />

Braun and others, resulting in the launch <strong>of</strong> Explorer 1,<br />

the first American satellite.<br />

HOPE (H-2 Orbital Plane)<br />

A Japanese unmanned space plane that would be<br />

launched by an H-2 booster and used <strong>to</strong> ferry materials <strong>to</strong><br />

and from the International Space Station. <strong>The</strong> project<br />

has not yet progressed beyond the stage <strong>of</strong> flight-testing<br />

subscale models.<br />

Length: 16.5 m<br />

Maximum diameter: 5.0 m<br />

Mass<br />

Total: 13,000 kg<br />

Payload: 2,000 kg<br />

Propellant: 1,000 kg<br />

horizontal preflight checkout<br />

A checkout accomplished with the vehicle in a horizontal<br />

position, thereby reducing the requirements for<br />

gantries, cranes, and similar items. Upon completion, the<br />

vehicle is erected in<strong>to</strong> vertical firing position. This kind<br />

<strong>of</strong> testing is generally used with smaller vehicles and<br />

spacecraft.<br />

hot test<br />

A propulsion system test that is carried out by actually<br />

firing the propellants.<br />

HOTOL (Horizontal Take<strong>of</strong>f and Landing vehicle)<br />

A British design, conceived by Alan Bond, for a singlestage-<strong>to</strong>-orbit<br />

winged launch vehicle using a unique airbreathing<br />

engine design. <strong>The</strong> RB545 air/liquid hydrogen/<br />

liquid oxygen (LOX) engine was <strong>to</strong> be developed by Rolls-<br />

Royce. Work on HOTOL began in 1982 by a Rolls-<br />

Royce/British Aerospace team and had reached the stage<br />

<strong>of</strong> detailed engine design and mockup when, in the mid-<br />

1980s, the British government withdrew further funding.<br />

HOTOL would have taken <strong>of</strong>f horizontally with a rocketpropelled<br />

trolley, switched <strong>to</strong> pure rocket propulsion at<br />

Mach 5 or 6, ascended <strong>to</strong> orbit, and glided back <strong>to</strong> Earth<br />

like the Space Shuttle <strong>to</strong> a runway landing. <strong>The</strong> HOTOL<br />

airframe was derived from conventional vertical take<strong>of</strong>f<br />

rockets with the engines mounted at the rear <strong>of</strong> a blunt<br />

based fuselage. Since such a vehicle’s empty center <strong>of</strong><br />

gravity is dominated by the location <strong>of</strong> the engine, the<br />

wings and the tank for the dense LOX also had <strong>to</strong> be at the<br />

rear. <strong>The</strong> payload bay and hydrogen tankage were placed<br />

in a projecting forebody. <strong>The</strong> resulting configuration suffered<br />

from a severe center <strong>of</strong> pressure/center <strong>of</strong> gravity<br />

mismatch during the air breathing ascent. <strong>The</strong> center <strong>of</strong><br />

pressure shifted 10 m forward due <strong>to</strong> the wide Mach range,<br />

the large fuselage cross-section-<strong>to</strong>-wing area ratio, and the<br />

long overhang <strong>of</strong> the forward fuselage. Various design<br />

changes were made <strong>to</strong> address these problems, all <strong>of</strong> which<br />

eroded the payload. Conventional landing gear was<br />

replaced by a specially designed take<strong>of</strong>f trolley <strong>to</strong> improve<br />

the marginal payload fraction. <strong>The</strong> final design had serious<br />

operational disadvantages and a small payload, and the<br />

only way the designers could continue <strong>to</strong> claim <strong>to</strong> put a<br />

reasonable payload in<strong>to</strong> orbit was by specifying untried<br />

and speculative structural materials. HOTOL subsequently<br />

evolved in<strong>to</strong> Skylon, which is being developed by<br />

Bond and his colleagues at Reaction Engines.<br />

Length: 75.0 m<br />

Core diameter: 7.0 m<br />

Lift<strong>of</strong>f thrust (from 3 engines): 3,153,200 N<br />

Mass: 250,000 kg (<strong>to</strong>tal), 50,000 kg (empty)<br />

housekeeping<br />

Routine tasks required <strong>to</strong> maintain spacecraft in habitable<br />

and/or operational condition during flight.<br />

Hubble Space Telescope (HST)<br />

An orbiting observa<strong>to</strong>ry built and operated jointly by<br />

NASA and ESA (European Space Agency), and named<br />

for the American astronomer Edwin Hubble (1889–<br />

1953). It has a 2.4-m-diameter main mirror and, following<br />

upgrades and repairs since its launch, is equipped<br />

with the Wide-Field and Planetary Camera 2 (WFPC-2),<br />

the Near Infrared Camera and Multi-Object Spectrometer<br />

(NICMOS), the Space Telescope Imaging Spectrograph<br />

(STIS), and, most recently installed, the Advanced<br />

Camera for Surveys (ACS).<br />

During initial on-orbit checkout <strong>of</strong> Hubble’s systems, a<br />

flaw in the telescope’s main reflective mirror was found<br />

that prevented the proper focusing <strong>of</strong> incoming light—a<br />

problem caused by the incorrect adjustment <strong>of</strong> a testing<br />

device used while building the mirror. Fortunately, Hubble<br />

was designed for regular on-orbit maintenance by the<br />

Space Shuttle. <strong>The</strong> first servicing mission, STS-61 in December<br />

1993, fully overcame the problem by installing a<br />

corrective optics package and upgraded instruments. A second<br />

servicing mission, STS-82 in February 1997, installed<br />

two new instruments in the observa<strong>to</strong>ry, and a third, STS-<br />

103 in December 1999, replaced Hubble’s six gyros. <strong>The</strong><br />

most recent Shuttle visit <strong>to</strong> Hubble, STS-109 in March<br />

2002, was <strong>to</strong> install the ACS and refurbish the NICMOS.<br />

<strong>The</strong> program includes significant participation by<br />

ESA, which provided one <strong>of</strong> the science instruments, the

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