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.

tachyon<br />

A hypothetical particle that travels faster than the speed<br />

<strong>of</strong> light. <strong>The</strong> existence <strong>of</strong> tachyons is allowed in principle<br />

by Einstein’s special theory <strong>of</strong> relativity; however, all<br />

attempts <strong>to</strong> detect them <strong>to</strong> date have been unsuccess-<br />

95, 241 ful.<br />

Taifun<br />

Second-generation Soviet target and surveillance satellites<br />

used for testing air defense and space tracking systems.<br />

<strong>The</strong> Taifun-1 series consisted <strong>of</strong> nearly 40 spacecraft<br />

launched from the mid-1970s onward. Taifun-2 satellites,<br />

<strong>of</strong> which some 30 were launched between 1976 and<br />

1995, differed from their predecessors in the type <strong>of</strong><br />

equipment carried and also in the fact that they released<br />

up <strong>to</strong> 25 Romb subsatellites. All the Taifun spacecraft<br />

were placed in<strong>to</strong> low Earth orbits <strong>of</strong> high inclination<br />

using Cosmos-3M launch vehicles from Plesetsk and<br />

Kapustin Yar.<br />

Taiyo<br />

A Japanese satellite designed <strong>to</strong> study how solar ultraviolet<br />

and X-rays affect Earth’s thermosphere. Taiyo (“sun”)<br />

is also known as Shinsei-3 and SRATS (Solar and <strong>The</strong>rmospheric<br />

Radiation Satellite).<br />

Launch<br />

Date: February 24, 1975<br />

Vehicle: M-3C<br />

Site: Kagoshima<br />

Orbit: 255 × 3,135 km × 31°<br />

Mass: 86 kg<br />

T<br />

Tansei Series<br />

428<br />

Taiyuan Satellite Launch Center (TSLC)<br />

A Chinese launch center, also known as Wuzhai, located<br />

in Shanxi province (37.5° N, 112.6° E). It is used <strong>to</strong><br />

launch missions with highly inclined (polar) orbits.<br />

take<strong>of</strong>f mass<br />

<strong>The</strong> mass <strong>of</strong> a launch vehicle, including all stages, fuel,<br />

and payload, at the time <strong>of</strong> take<strong>of</strong>f.<br />

Tanegashima Space Center<br />

A Japanese launch site on the island <strong>of</strong> Tanegashima<br />

(30.2° N, 130.9° E), 980 km southwest <strong>of</strong> Tokyo. It is<br />

the largest such facility in Japan and is used for missions<br />

<strong>of</strong> NASDA (National Space Development Agency).<br />

Launches from here are normally restricted <strong>to</strong> two 90-day<br />

windows per year, due <strong>to</strong> safety range procedures set up<br />

as a result <strong>of</strong> pressure from local fishermen.<br />

Tansei<br />

A series <strong>of</strong> small Japanese satellites, launched from<br />

Kagoshima, designed <strong>to</strong> test the performance <strong>of</strong> new<br />

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

launch vehicles. (See table, “Tansei Series.”)<br />

Taurus<br />

A four-stage launch vehicle that uses the same Orion<br />

solid mo<strong>to</strong>r combination as its smaller cousin, the Pegasus,<br />

stacked on <strong>to</strong>p <strong>of</strong> a larger Cas<strong>to</strong>r 120 solid mo<strong>to</strong>r.<br />

First flown in 1994, the Taurus stands 27 m tall, weighs<br />

69,000 <strong>to</strong> 101,000 kg at ignition, and is easily transported<br />

and launched. It was designed <strong>to</strong> extend Orbital Sciences’<br />

ability <strong>to</strong> launch small and Med-Lite satellites. Four variants<br />

<strong>of</strong> the Taurus launch vehicle exist. <strong>The</strong> smallest,<br />

known as the ARPA Taurus, uses a Peace Keeper first<br />

Launch<br />

Spacecraft Date Vehicle Orbit Mass (kg)<br />

Tansei Feb. 16, 1971 M-4S 990 × 1,110 km × 30° 63<br />

Tansei-2 Feb. 16, 1974 M-3C 290 × 3,240 km × 31° 56<br />

Tansei-3 Feb. 19, 1977 M-3H 790 × 3,810 km × 31° 129<br />

Tansei-4 Feb. 17, 1980 M-3S 521 × 606 km × 39° 185

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

Saved successfully!

Ooh no, something went wrong!