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SN User's Guide - ESC Home - NASA

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systems of other services which are also allocated on a primary basis. New systems<br />

cannot be introduced into that frequency band if they will result in interference to a<br />

system operating with a primary allocation. A secondary allocation to a service allows<br />

systems to operate in a band on the condition that it does not cause interference to, nor<br />

claims protection from, systems operating on a primary basis. However, systems<br />

operating on a secondary basis can claim protection from interference from other<br />

systems operating on a secondary basis.<br />

D.3.2 Consequences of Exceeding PFD Limits<br />

If the PFD levels do not meet the PFD limits given in the NTIA manual, the NTIA will not<br />

grant frequency authorization except as noted in paragraph D.3.1.<br />

If the PFD levels do not meet the PFD limits given in the ITU-R RR, then the mission is<br />

subject to the conditions given in Article 4.4. Article 4.4 states “Administrations of the<br />

Member States shall not assign to a station any frequency in derogation of either the<br />

Table of Frequency Allocations in this Chapter or the other provisions of these<br />

Regulations, except on the express condition that such a station, when using such a<br />

frequency assignment, shall not cause harmful interference to, and shall not claim<br />

protection from harmful interference caused by, a station operating in accordance with<br />

the provisions of the Constitution, the Convention and these Regulations.”<br />

D.3.3 Calculation of PFD Levels<br />

The calculation of PFD levels requires the following data for the spacecraft:<br />

a. Maximum transmitter power contained in the reference bandwidth (i.e., 4 kHz or<br />

1 MHz), under all conditions and modes of modulation measured at the antenna<br />

input. Please see paragraph D.3.3.1 below.<br />

b. Transmitting antenna gain pattern.<br />

c. Transmitting antenna mainbeam pointing characteristics, including any<br />

intentional or unintentional antenna mispointing.<br />

d. Orbital altitude (nominally circular orbits are assumed for this analysis).<br />

The PFD at an angle of arrival, α, is calculated as shown in<br />

Equation D-1Equation D-1 with R(α) found using Equation D-2 and Equation D-3. The<br />

geometry is shown in Figure D-1:<br />

Equation D-1:<br />

where:<br />

<br />

Gt ( ) PtB<br />

<br />

PFD ( )<br />

= 10 log <br />

2 <br />

4πR<br />

( )<br />

<br />

Revision 10 D-4 450-<strong>SN</strong>UG

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