Page 207 - Intro to Space Sciences Spacecraft Applications
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Introduction to Space Sciences and Spacecraft Applications
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                                                 Table 8-10
                                        United States Launch Vehicles*
                                       Launch             Lift-off          Low-orbit
                                     Weight (Ibs)       Thrust (Ibs)       Payload (Ibs)
                     Delta              426,000           63 1,100            6,000
                     Atlas              292,600           37 8,000            11,200
                     Titan             15 19,600        2,920,000            34,050
                     Shuttle          4,500,000          6,425,000           65,000
                     *Typical perJormances of the mast common US. launch vehicles are given.


                     upper stage is a separate rocket which is usually separated from the space-
                     craft after use.
                        An important point is that if  an upper stage is required, it usually sub-
                     tracts from the available weight and space for the payload in the launch
                     vehicle. (Because launch vehicles are multistage rockets, some of the final
                     stages may be capable of delivering the payload into the desired orbit with-
                     out the use of an additional upper stage.) Some common upper stages are
                     the liquid-fueled  Centaur (used to  send the Viking and Voyager probes
                     away from the earth), and the solid-fueled Payload Assist Module (PAM)
                     and Inertial Upper Stage (IUS), both capable of use from the space shuttle.

                     Ground Sites

                        Ground sites consist of the spacecraft control facilities, which monitor and
                     task the system in orbit, and the receiving sites to which the spacecraft may
                      transmit information for dissemination and use. These are many and varied
                      and depend on the operator of the spacecraft. At the receiving sites, infor-
                      mation is collected and put into a form suitable for dissemination to the users.
                        On the ground is also the most important component of  a complete
                      space system: the system user. In many cases, the user drives the system
                      design and later operation, as indicated in Table 8- 11 which illustrates the
                      generic personality of communication, navigation, remote sensing, and
                     planetary systems. In many instances, the user only accesses the informa-
                      tion for whatever purpose the spacecraft was designed in the first place.
                      The task force commander at sea only knows that he has instant access to
                      his units, via the satellite communications link, and knows his and others’
                     positions accurately due to the availability of satellite navigation. Weath-
                     er information in his area of operations is provided by weather processing
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