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SN User's Guide - ESC Home - NASA

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Equation A-5<br />

Predicted Required Prec = Ideal Required Prec - L - Lp - LI - Lnc<br />

where:<br />

L = pointing loss (in dB) due to the inability of the customer platform to<br />

point its antenna directly at the TDRS (L 0 dB).<br />

Lp = polarization loss (in dB) due to mismatch of the customer platform<br />

radiated polarization and that of the TDRS receiving antenna (LP 0<br />

dB).<br />

LI, Lnc = RFI and customer platform incompatibility factors (in dB) as<br />

determined by CLASS (refer to paragraph 3.5.2) (LI 0 dB, Lnc 0<br />

dB).<br />

A.4.4<br />

By extension, the minimum customer platform EIRP, (EIRP)min, required to produce the<br />

predicted required Prec is as follows:<br />

Equation A-6<br />

(EIRP)min = Predicted Required Prec - Ls<br />

where: Ls is space loss as defined in paragraph A.3.2.<br />

A.4.5<br />

The return service performance margin M (in dB) is a customer decision that should be<br />

coordinated with GSFC Code 450 and should consider long-term performance<br />

degradation of the customer platform throughout its operational lifetime. M is defined as<br />

follows:<br />

Equation A-7<br />

M = EIRP - (EIRP)min (M > 0 dB)<br />

A.4.6<br />

The return service performance curves in Figure A-8 through Figure A-42 show ideal<br />

required (Prec) versus ADR for selected services, type of tracking and/or field of view,<br />

codings, modes, data rates and channels. Figure A-43 shows an example ADR versus<br />

customer platform EIRP for a hypothetical customer platform, for an assumed<br />

performance margin, M, as illustrated in Equation A-7. The service, coding, mode, and<br />

channel in Figure A-43 are assumed to be those given in Figure A-15, so as to illustrate<br />

how the predicted required Prec is realized, (or alternatively, how the ideal required Prec<br />

plus performance margin is realized).<br />

Revision 10 A-12 450-<strong>SN</strong>UG

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