19.07.2013 Views

JP 3-50 National Search and Rescue Manual Vol I - US Navy

JP 3-50 National Search and Rescue Manual Vol I - US Navy

JP 3-50 National Search and Rescue Manual Vol I - US Navy

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

APPENDIX E. COORDINATED SEARCH PATTERNS<br />

A. Coordinated Patterns<br />

This appendix provides OSCs with a guide for planning <strong>and</strong> executing<br />

coordinated search patterns. Teaming an aircraft with a vessel takes<br />

advantage of each SRU's best features. Aircraft provide rapid coverage<br />

of the search area from a good search platform. Vessels may provide<br />

better navigation, unless the aircraft is equipped with sophisticated<br />

navigational aids such as INS, <strong>and</strong> may be able to quickly rescue a<br />

survivor sighted from the aircraft.<br />

B. Coordinated <strong>Search</strong> Symbology<br />

The following symbols <strong>and</strong> definitions are used in computing <strong>and</strong><br />

discussing aircraft search tracks.<br />

Al is the search area length.<br />

Aw (search area width) is the sum of one searchleg <strong>and</strong> one track<br />

spacing (Aw = L + S).<br />

Awf is the search area width for faster aircraft in CMCS pattern.<br />

Aws is the search area width for slower aircraft in a CMCS pattern.<br />

C (course) is the intended path of travel by an SRU.<br />

GS (ground speed) is the speed of an aircraft relative to the<br />

earth's surface.<br />

H (heading) is the horizontal direction in which an SRU is<br />

pointing.<br />

L (searchleg or searchleg length) is the sum of the searchleg<br />

straightaway (y) <strong>and</strong> the search craft's turn diameter (TD). Subscripts<br />

further define L.<br />

L1 is the searchleg with the highest headwind component.<br />

L2 is the searchleg with the highest tailwind component.<br />

S (track spacing) is the distance between adjacent searchlegs.<br />

t1 is the time required for a search aircraft to fly one-half of<br />

the straightaway length (Y1) of the searchleg with the highest headwind<br />

component (L1).<br />

t2 is the time required for a search aircraft to fly one-half of<br />

the straightaway length (y2) of the searchleg with the highest tailwind<br />

component (L2).<br />

t3 is the time required for a search aircraft to fly the full

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!