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SN User's Guide - ESC Home - NASA

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and an ephemeris uncertainty as defined in Table 6-9. This value applies at the<br />

carrier tracking threshold. The carrier tracking threshold for DG1 signals is a<br />

minimum Prec of -201.4 dBW or the minimum Prec for BER, whichever is greater.<br />

The carrier tracking threshold for DG2 signals is a minimum Prec of -195.3 dBW<br />

or the minimum Prec for BER, whichever is greater.<br />

6.3.3.4 Reacquisition<br />

While in the PN/carrier tracking state, a loss of lock condition induced by a cycle slip will<br />

be automatically detected and a reacquisition will be automatically initiated. For a<br />

customer platform that continues to transmit the minimum Prec for acquisition and<br />

maintains with an ephemeris uncertainty as defined in Table 6-9, the normal total<br />

channel reacquisition time for either powered or non-powered flight dynamics will be<br />

less than or equal to that for the initial total channel acquisition for non-powered flight<br />

dynamics, with a probability of at least 0.99. If lock is not achieved within 10 seconds of<br />

loss of lock, an acquisition failure notification will be sent to the MOC and the <strong>SN</strong> ground<br />

terminal will reinitiate the initial service acquisition process. TDRSS SSA return service<br />

does not support acquisition of customers with powered flight dynamics. Upon receipt<br />

of the loss-of-lock indications in the UPD, the customer MOC may request a TDRSS<br />

SSA return service reacquisition GCMR (refer to Section 10). It is recommended that<br />

the customer MOC delay initiation of the GCMR for at least 35 seconds after initial<br />

receipt of the loss-of-lock indications in the UPD.<br />

6.3.3.5 Additional Service Restrictions<br />

a. Sun Interference. The TDRSS SSA return service performance will not be<br />

guaranteed when the center of the sun is within 4 degrees of the TDRS SSA<br />

receiving antenna boresight; however, this sun interference checking is a<br />

customer MOC responsibility. Additionally, the TDRSS SSA return service<br />

performance will not be guaranteed when the center of the sun is within<br />

1 degree of the boresight of the <strong>SN</strong> ground terminal receiving antenna<br />

supporting the TDRS.<br />

b. Frequency and Polarization. The TDRSS SSA return service can support the<br />

customer platform with assigned frequencies anywhere within the 2200 to 2300<br />

MHz band with either RHC or LHC polarization. The following restrictions<br />

apply:<br />

1. The BER relationships of Table 6-9 are satisfied for center frequencies<br />

from 2205 to 2295 MHz (refer to Appendix D for power level restrictions<br />

into the 2290-2300 MHz band and <strong>NASA</strong>/GSFC Recommended Filtering).<br />

For customer center frequencies below 2205 MHz or center frequencies<br />

above 2295 MHz, acceptable data service may be achieved when the<br />

customer’s spectrum does not spill over the edges of the 2200 to 2300<br />

MHz band.<br />

2. The customer platform spectrum should be constrained so that the first<br />

null of the spectrum falls within the 2200 to 2300 MHz band.<br />

3. In addition, the customer platform should consider employing selectable<br />

polarization capability.<br />

Revision 10 6-35 450-<strong>SN</strong>UG

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