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TYPICAl TANKER ORBIT PATTERN<br />

THE COMBAT TALON WEAPONS SYSTEM<br />

Ilj.hl I -V.Y' irP'1^11 lEM ■<br />

POINT PARALLI£L HE1>JDEZV0US PROFrLE<br />

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Figure 24. Typical Point-Parallel Procedure (Source: TO 1-1C-1-29, “Flight Crew Air Refueling Procedures with KC-135 and<br />

KC-10,” 1 February 1977.)<br />

fuel from the main tanks into the externals to get<br />

a full external tank indication. Because of the<br />

inability to fuel the external tanks fully while<br />

connected to the tanker, operators were advised<br />

to plan for a total fuel quantity of 56,000 pounds<br />

after refueling. <strong>The</strong> point-parallel rendezvous<br />

procedure was used during two rejoins using the<br />

briefed 12 NM turn range and approximately 4.5<br />

NM offset. <strong>The</strong> procedure worked perfectly, and<br />

it was recommended for use throughout the Combat<br />

Talon community. <strong>The</strong> 1st SOS crew that<br />

flew the long-range mission included Steve<br />

Gardella, AC/SQ CC; Bob Meller, FP; Jerry<br />

Nichols, FP; Jack Holbein, NAV; Joe McBride,<br />

NAV; Paul Whetzel, NAV; Rueben Cole, FE;<br />

“Rat” Moretz, FE; Chuck Javens, RO; John Mink,<br />

RO; Ray Doyle, LM; and John Stumpf, LM.<br />

To fly anywhere in the world without relying<br />

on ground-based aerial refueling was a reality.<br />

No longer did the United States have to rely on<br />

other nations to provide refueling support facilities<br />

that were subject to political pressures. <strong>The</strong><br />

modern-day Combat Talon weapons system was<br />

nearly complete.<br />

<strong>The</strong> Helicopter Aerial-Refueling<br />

Modification<br />

By the mid-1980s the number of military helicopters<br />

with in-flight refueling capability had increased<br />

significantly over the previous decade.<br />

<strong>The</strong> medium-lift special operations helicopter,<br />

the MH-53 Pave Low, formed the backbone of the<br />

USAF SOF rotary-wing capability. A smaller,<br />

light-lift helicopter, the MH-60G Pave Hawk,<br />

also provided specialized SOF rotary-wing support.<br />

With Congress’s passing of the Goldwater–<br />

Nichols Department of Defense Reorganization<br />

Act of 1986, renewed emphasis was placed on<br />

America’s SOF forces. As part of the SOF avia -<br />

tion modernization program that was developed<br />

after the act, both USAF and USA aircraft were<br />

provided increased capabilities, including aerial<br />

refueling for USA Chinook helicopters dedicated<br />

to SOF support. Just as planners a decade<br />

before had recognized the need to install inflight<br />

aerial refueling receiver capability on the<br />

Combat Talon, SOF rotary-wing assets were<br />

modified, or designed from the ground up, with<br />

the capabilit y to receive fuel while airborne. <strong>The</strong><br />

55

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