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SIGMA TANDEM SYSTEM OWNER’S MANUAL
11301 - 00.00.0000
Section 1: The Sigma Tandem System • Chapter 1 - New Features
will always be where you expect them to be. There is no more stowing of loose handles after
opening, and no more looking for handles at packing time. For further security, each ripcord handle
is countersunk, so that it snugly slides 3/8 of an inch over the end of its housing. Each ripcord has
3 inches of slack built in, so that it takes a 5- inch pull, on either handle, to release the drogue.
THE SAFETY PIN
(PATENT PENDING)
The system also incorporates a special “safety pin” on the drogue bridle, which locks the main container pin in place
until the drogue is deployed. On all other systems, if you snag a drogue release ripcord moving around the aircraft,
or on exit, or if you accidentally pull the wrong handle after exit, you end up with a main canopy as soon as you throw
your drogue. The unique safety pin prevents this scenario.
HOW THE SYSTEM WORKS
In tandem, the force exerted by the deployed drogue at terminal velocity is roughly equal to half of the suspended
weight. This force, transferred through the disk, is shared (divided) equally by the four main container flaps. Because
both ends of the container closing loop are attached to the same (bottom) flap, the closing pin end of the loop only
receives half of the force exerted on the bottom flap, or one-eighth of the total force exerted by the drogue. So, if the
drogue deployed above a 400 pound tandem pair exerts a force of 200 pounds on the disk, then the container closing
pin receives one-eight, or 25 pounds of force. A stainless steel pin, moving through a Spectra loop, over a stainless
steel grommet, has a mechanical advantage of about five to one. So a pull of 5 pounds is all that is necessary to move
the pin. But, the Spectra ripcords are set up as 2-1 pulleys, so theoretically a force of only 2½ pounds at the ripcord
handle should move the pin. However, tension from the bungee recoil system, plus eyelet and housing friction, add
about 7 pounds of resistance back into the equation, yielding a total pull force, at the handle, of about 10 pounds.
A NEW DROGUE
(PATENT PENDING)
While the drogue canopy is essentially unchanged, the bridle and kill line have been redesigned. The 1¾ ” Kevlar outer
bridle extends past the disk all the way to the main deployment bag. The kill line is now 1,000 lb. Vectran/Spectra and
also terminates at the bag. Because the lower ends of both the bridle and the kill line end at the same place, it is
impossible to twist one independently of the other. This means no more time consuming untwisting of the kill line.
Because both bridles are now made of non-stretch materials, no “stop ring” is required on the inner bridle. This means
less wear, and that the kill line can be easily replaced in the field. And because both the bridle and the kill line share the
bag lift-off forces (On all other systems either the kill line or outer bridle takes it all alone) if either the bridle or the kill
line breaks, deployment still happens more or less normally, and you don’t lose your expensive drogue.
A NEW MAIN DEPLOYMENT BAG
The Sigma Tandem main deployment bag has also been redesigned, eliminating the grommet at the top of the bag,
and replacing it with a continuous loop of tubular nylon. This prevents canopy damage caused by trapping canopy
fabric between the bag’s grommet and the canopy attachment point.
Summary of Contents for TANDEM VECTOR
Page 1: ......
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Page 6: ...CHAPTER 1 THESIGMA TANDEMSYSTEM CHAPTER 1 THESIGMA TANDEMSYSTEM...
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Page 12: ...CHAPTER 2 APPLICANT COURSE INFORMATION CHAPTER 2 APPLICANT COURSE INFORMATION...
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Page 19: ...CHAPTER 1 DESCRIPTION CHAPTER 1 DESCRIPTION...
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Page 32: ...CHAPTER 2 OPERATION CHAPTER 2 OPERATION...
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Page 39: ...CHAPTER 3 RESERVE CONTAINER CHAPTER 3 RESERVE CONTAINER...
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Page 72: ...CHAPTER 4 MAINCONTAINER CHAPTER 4 MAINCONTAINER...
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Page 106: ...CHAPTER 1 PREPARATION CHAPTER 1 PREPARATION...
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Page 115: ...CHAPTER 2 IN AIRCRAFT EXITS...
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Page 119: ...CHAPTER 3 FREEFALL DROGUE FALL CHAPTER 3 FREEFALL DROGUE FALL...
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Page 126: ...CHAPTER 4 CANOPY CONTROL CHAPTER 4 CANOPY CONTROL...
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Page 132: ...CHAPTER 1 RESERVE PROCEDURES CHAPTER 1 RESERVE PROCEDURES...
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Page 136: ...CHAPTER 2 AIRCRAFT EMERGENCIES STUDENT REFUSAL CHAPTER 2 AIRCRAFT EMERGENCIES STUDENT REFUSAL...
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Page 140: ...CHAPTER 3 FREEFALL CHAPTER 3 FREEFALL...
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Page 146: ...CHAPTER 4 CANOPY CONTROL CHAPTER 4 CANOPY CONTROL...
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Page 151: ...CHAPTER 1 STUDENTSKILLS FORFIRSTJUMP CHAPTER 1 STUDENTSKILLS FORFIRSTJUMP...
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Page 156: ...CHAPTER 2 OTHER ACTIVITIES CHAPTER 2 OTHER ACTIVITIES...
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Page 160: ...APPENDIX...
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