Attachment Schedule S GXT

This document pretains to SAT-LOA-20080509-00101 for Application to Launch and Operate on a Satellite Space Stations filing.

IBFS_SATLOA2008050900101_640986

EXHIBIT 5K: BACK—UP COMMAND BEAM [BICONE/OMNI ANTENNA] Beam Polarization: Right Hand Circular Peak Antenna Gain: —2.3 dBi Peak G/T:; —35.6 dB/K Command Threshold Flux Density at Peak G/T: —89.7 dBW/m* (Schedule S Beam Designation: CMDO) _ (a) Elevation Cut Antenna Gain Pattern v:‘.(r d . i,#__\ $o i_ | i o t oo ocoBc j 123 94 6 3 — shoLs, bea Notes: 1) Gain variation in elevation shown for the azimuth angle of 0°. 2) The x—axis represents the elevation angle and spans from —180° to +180°. Each major axis division line represents 20° ofelevation. 3) The y—axis represents the antenna gain. Each major axis division linerepresents 2 dB of gain: (b) Azumuth Cut Antenna Gain Pattern _ *T\ Eain Hohnk q.i day | GE _rn@p — [ ¥ 1? . ".fim ul _ K.. _ o §° in[ ' ts (Ef —E at— >) | |s Op up UA oi l0| 501 01 U s s to fasgo ut o 1 on tao d3 L+K ho igt Bo . D ar m 0 ho . ANGLE, CEG Notes: 1) Gainvariationin azimuth shown for elevation angles of 0° and £+20°. 2) The x—axis represents the azimuth angle and spans from 180°to +180°. Each major axis division line represents 20° of azimuth. 3) The y—axis represents the antenna gain. Each major axis division line represents 2 dB of gain. Page 46 of 68


Document Created: 2019-04-15 06:11:49
Document Modified: 2019-04-15 06:11:49
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