1 - The Black Vault
1 - The Black Vault
1 - The Black Vault
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PRAETORIAN STARSHIP<br />
that everyone in front of the navigator’s curtain<br />
use NVGs. <strong>The</strong> right-seat pilot flew the approach<br />
with panel lights turned out, while the flight engineer<br />
monitored the engine instruments and the<br />
right-seat pilot’s approach. Both the right-seat pilot<br />
and the flight engineer focused their NVGs<br />
inside the cockpit. To prevent any light bleeding<br />
forward from the navigators’ station, heavy blackout<br />
curtains were installed in place of the thin<br />
dividing curtain used on standard C-130 aircraft.<br />
All lights forward of the curtain were either<br />
turned off or taped to prevent illuminating the<br />
interior of the cockpit. Throughout the approach<br />
the left-seat pilot and the third pilot (safety pilot)<br />
focused their NVGs outside the aircraft and<br />
scanned for the runway environment. At one to<br />
four miles out from landing, the left-seat pilot acquired<br />
the landing lights, the safety pilot confirmed<br />
them, and the left-seat pilot began flying<br />
the aircraft. Airspeed, absolute altitude, and<br />
vertical-velocity information were read to the leftseat<br />
pilot by the right-seat pilot and the left navigator<br />
until the aircraft touched down on the runway.<br />
If no lights were on the runway, the left-seat<br />
pilot usually acquired the runway within a mile of<br />
the approach end, depending on moon illumination<br />
and the brightness of the runway striping. As<br />
the aircraft decelerated through 40 knots after<br />
landing, the landing lights were turned off, and<br />
the aircraft rolled out to its predetermined offload<br />
location. Covert taxi lights were used sparingly<br />
and usually only during turns or in congested<br />
areas. 1<br />
For NVG takeoffs the left-seat pilot maintained<br />
runway alignment with visual reference to the<br />
runway centerline while still using NVGs. <strong>The</strong><br />
right-seat pilot read off the airspeeds as the aircraft<br />
accelerated. On rotation the right-seat pilot<br />
provided the left-seat pilot with the number of<br />
degrees nose-up attitude and the aircraft’s airspeed<br />
on climb out. With the introduction of the<br />
IR filters for the aircraft lights and for the portable<br />
runway lights, Vaught’s requirement for total<br />
blacked-out landings (to the naked eye) was<br />
achieved. 2<br />
Fuel-Cell (Blivet) Airdrop<br />
<strong>The</strong> 8th SOS had initially identified the need<br />
to air-drop fuel to helicopters during the October<br />
1979 Red Flag exercise held at Nellis AFB, Nevada.<br />
When the requirement to refuel helicopters<br />
arose in late November, JTF planners turned to<br />
the air-drop method as their first solution to the<br />
refueling problem. <strong>The</strong> initial blivet drop was<br />
conducted using rigging similar to the CRRC,<br />
with two G-12D parachutes to support a rigged<br />
weight of 3,500 pounds (500 gallons of fuel). As<br />
the number of helicopters were expanded to six,<br />
then later to eight, the number of blivets to be<br />
dropped by each C-130 increased to five. Between<br />
December 1979 and February 1980, the blivet<br />
drop was refined to include all equipment required<br />
to position the blivets and then to pump<br />
fuel to the waiting helicopters. Thus, the standard<br />
five-blivet airdrop included two petroleum,<br />
oil, and lubricant pumps (A-22s) and a small<br />
tractor, called a mule, to move the blivets into<br />
position. <strong>The</strong> total weight of the load was approximately<br />
20,000 pounds. 3<br />
Testing was done on the five blivet loads at<br />
Fort Bragg and at Yuma, Arizona, in December<br />
and in early 1980. Testing confirmed that CDS<br />
procedures provided were the most accurate and<br />
effective means to deliver the heavy load. <strong>The</strong> following<br />
modifications were made to the Combat<br />
Talon to allow for successful CDS air-drops:<br />
1. Additional intermediate rails were installed.<br />
2. A dual CDS gate (strap with cutter blade)<br />
was developed.<br />
3. Retractable VanZelm ratchets were installed.<br />
4. Individual gates were used for each blivet.<br />
Although the fuel blivet air-drop procedure<br />
was not used for the actual mission, the air-drop<br />
option remained the JTF’s first choice until<br />
shortly before mission execution. A secondary<br />
airland method of delivering the blivets also was<br />
developed. Called the blivet combat off-load, it<br />
included modification of the ground-loading<br />
ramps with skate wheels to allow the aircraft to<br />
taxi with the loading ramps deployed. After the<br />
aircraft had landed and taxied to its off-load loca -<br />
tion, each blivet would be released from its restraints<br />
one at a time as the aircraft taxied forward.<br />
After the first blivet was downloaded, the<br />
aircraft would stop, the loadmaster would cut the<br />
second blivet loose, and the aircraft would<br />
resume taxi while the blivet exited the rear of the<br />
aircraft. <strong>The</strong> procedure was repeated until all<br />
blivets were unloaded. At Desert One Fleming’s<br />
crew downloaded three fuel blivets using the<br />
combat off-load procedure. 4<br />
Fuel-Bladder Refueling System<br />
Although airdrop of the fuel blivets proved to<br />
be a viable delivery technique, the Delta Force<br />
commander, Col Charlie Beckwith, did not like<br />
the idea of having to depend on air-dropped<br />
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