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

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stage instead <strong>of</strong> a Cas<strong>to</strong>r 120 mo<strong>to</strong>r. <strong>The</strong> standard Taurus<br />

uses a Cas<strong>to</strong>r 120 first stage and a slightly larger Orion<br />

50S-G second stage. <strong>The</strong> Taurus XL uses the Pegasus XL<br />

rocket mo<strong>to</strong>rs and is considered a development stage<br />

launch vehicle. <strong>The</strong> largest Taurus variant, the Taurus<br />

XLS, is a study phase vehicle that adds two Cas<strong>to</strong>r IVB<br />

solid rocket boosters <strong>to</strong> the Taurus XL <strong>to</strong> increase payload<br />

capacity by 40% over the standard Taurus. For all<br />

Taurus configurations, satellite delivery <strong>to</strong> a geostationary<br />

transfer orbit can be achieved with the addition <strong>of</strong> a<br />

Star 37FM perigee kick mo<strong>to</strong>r. Five consecutive launch<br />

successes for Taurus, from 1994 through 2000, were followed<br />

by a failure on September 21, 2001, in which the<br />

OrbView-4 and QuikTOMS satellites were lost.<br />

TDRSS (Tracking and Data Relay Satellite System)<br />

A constellation <strong>of</strong> geosychronous communications satellites<br />

and ground support facilities for use by the Space<br />

Shuttle and other low-Earth-orbiting spacecraft. When<br />

first launched, the TDRS satellites were the largest, most<br />

sophisticated communications satellites ever built. <strong>The</strong><br />

second vehicle in the series was lost in the Challenger<br />

disaster and later replaced by TDRS-7. TDRS-8 (H),<br />

-9 (I), and -J are higher performance replacements for the<br />

original satellites. (See table, “TDRS Series.”)<br />

Launch site: Cape Canaveral<br />

Maximum diameter: 3.4 m (s<strong>to</strong>wed), 21 × 13 m (solar<br />

panels and antennas deployed)<br />

Mass (TDRS-8 through -J, on-orbit): 1,781 kg<br />

Teledesic<br />

A communications system designed <strong>to</strong> provide broadband<br />

and Internet access, videoconferencing, and high-<br />

TDRS Series<br />

Telstar 429<br />

quality voice and other digital data services through a<br />

constellation <strong>of</strong> 288 satellites in low Earth obit. <strong>The</strong><br />

Teledesic network consists <strong>of</strong> terminals that interface<br />

between the satellite network and terrestrial end-users,<br />

network gateways, network operations and control systems<br />

that perform network management functions, and a<br />

space segment that provides the communication links<br />

and switching among terminals. Teledesic’s space-based<br />

network uses fast-packet switching <strong>to</strong> provide seamless,<br />

global coverage. Each satellite is a node in the fast-packetswitch<br />

network and communicates through crosslinks <strong>to</strong><br />

other satellites in the same and adjacent orbital planes.<br />

Communications are treated within the network as<br />

streams <strong>of</strong> short, fixed-length packets. Each packet carries<br />

the network address <strong>of</strong> the destination terminal, and each<br />

node independently selects the least-delay route <strong>to</strong> that<br />

destination. <strong>The</strong> Teledesic Network is planned <strong>to</strong> begin<br />

operations in 2003. Teledesic 1, the first satellite in the<br />

constellation, was launched on February 26, 1998, by a<br />

Pegasus XL from Vandenberg Air Force Base.<br />

telemetry<br />

Data received electronically from a spacecraft during<br />

flight. Telemetry informs ground control about the condition<br />

<strong>of</strong> the crew and <strong>of</strong> various critical parts and functions<br />

<strong>of</strong> the spacecraft.<br />

Telstar<br />

A global network <strong>of</strong> communications satellites operated<br />

by AT&T Skynet, later Loral Skynet. Telstar 1 was the first<br />

commercial communications satellite; owned by AT&T<br />

and flown by NASA, it relayed the first transatlantic television<br />

transmissions between Andover, Maine, and stations<br />

in Goonhilly, England, and Pleumeur-Bodou,<br />

France. Telstar 8 was scheduled for launch in the third<br />

Spacecraft Date<br />

Launch<br />

Vehicle GSO Location<br />

TDRS-1 Apr. 4, 1983 Shuttle STS-6 49° W<br />

TDRS-3 Sep. 29, 1988 Shuttle STS-26 275° W<br />

TDRS-4 Mar. 13, 1989 Shuttle STS-29 41° W<br />

TDRS-5 Aug. 2, 1991 Shuttle STS-43 174° W<br />

TDRS-6 Jan. 13, 1993 Shuttle STS-54 47° W<br />

TDRS-7 Jul. 4, 1995 Shuttle STS-70 71° W<br />

TDRS-8 (H) Jun. 30, 2000 Atlas IIA 150° W<br />

TDRS-9 (I) Mar. 8, 2002 Atlas IIA n/a*<br />

*A problem with the satellite’s propellant supply after launch left it unclear, as <strong>of</strong> mid-<br />

2002, whether TRDS-9 could be raised <strong>to</strong> its intended orbit.

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