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Annex C ESM system<br />

C.1 Background<br />

An airhornc ESM system might providc a suitnhlc basis for<br />

a tacticnl communications or radar monitoring satellite.<br />

The basrlinc that will he assumcd here is he Kcstrcl Mk fl<br />

madc by HncalR. This is a radar ESM. capablc of dctcclhg.<br />

drintcrlcaving nnd tracking radar emissions hetwecn c and<br />

1 hnnd.<br />

C.2 Detection capability<br />

Kestrel employs a six port amplitudc comparison recciver<br />

to nicnsurc signal bearing. The standard antennas givc 360'<br />

covcrngc in azimuth. 25O covcragc in clcvnlion. a typical<br />

pulsc scnsitivity of -60 dRmi and bearing nccuracy of 4.5O<br />

RMS. This would dctcct the main lobc of a 10 MW E\tP C-<br />

hnn:l rnclnr nt n rnngc of SO0 km. It would also hc pc";sihlc<br />

to locatc thc radar to nn accuracy of approximatcly 5Okm<br />

h; uackinp thc hearing of thc radar as thc sntcllitc pas?:s.<br />

Antrnnas with grcatcr gain could hc uscd ut, thc ci:st of<br />

sncrifiring thc 360° capability. This would, hc ninrc cnsily<br />

achicvcd at higher frcqucncics antl it might' bc appropriate<br />

to rcplacc thc Rand 3 antcnna (I !o J hand) $id1 a multiple<br />

fccd horn and rcflrctor. A rcflcctiw of thc ordcr of 500 rnrn<br />

in diamctcr might bc cxpcctcd to givc 20 clR iniprovcmcnt<br />

in scnsitivity and a factor of Ifl improvcrncnt in hcaring<br />

accuracy hut would not add grcally to thc mass iir cost of<br />

the sy

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