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Length: |
5 feet, 2
inches |
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Diameter: |
2.685 inches |
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Weight: |
4.25 pounds
without motor |
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Motor: |
54mm mount
accommodates Hypertek 440cc tank and J-grain. |
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Altimeters: |
Adept ALTS-25
plus homemade G-switch timer as a back-up. |
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Locator: |
Walston radio
transmitter (mounted in the nose cone) |
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Payload: |
none |
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Parachute: |
Rocketman R7 |
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Built: |
Spring 1996 |
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First Flight: |
May 11, 1996
on J100 motor at Teapot Dome (Idaho) launch site |
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Construction: |
Body
tube: 2.6-inch diameter PML phenolic
Fins: 1/16-inch G10 fiberglass
Nose cone: plastic PML "intellicone"
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| Click on any photo to see a larger version of it. |
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My
hybrid rocket (a modified PML Tempest) is on the launch pad at Bonneville Salt
Flats during LDRS-17 in August of 1998. This rocket has a
Hypertek
motor system that burns liquid nitrous oxide (N20) as the oxidizer and ABS
black plastic as the fuel. It uses an Adept ALTS-2 altimeter for apogee
deployment. It also uses a home built G-switch timer for ejection
backup and a Walston transmitter for radio finding. (The Walston
unit was of course not needed at the Salt Flats. There is nothing there
for the rocket to hide behind!) |
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Lift-off of the PML Tempest on a J145 HyperTek Hybrid motor. This
motor produces very little smoke! There is also a complete lack
of tracking smoke once the motor burns out. Still it's a very nice
system and a little cheaper per flight than the solid propellant motors.
Peak altitude at Bonneville Salt Flats was 3139 feet.
I
don't have video of the PML Tempest flight, but I do have a very short
launch video of another hybrid rocket that is my modified RocketMan Hybrid
Dart. The video for that rocket (also on a J145 motor) is
available
here.
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Close up of my hybrid rocket
on my launch pad at LDRS-16 in Hartsel Colorado. You can see the fill
stem inserted into the motor to supply the nitrous oxide for filling the
on-board flight tank. The vent hole on the side of the rocket is where the
liquid nitrous will begin to vent once the on-board tank is full. Two small
hoses connect into fittings just below the horizontal blast deflector.
One hose supplies liquid nitrous and the other one supplies pure gaseous oxygen that is used to
ignite the motor. A high voltage transformer
is in the gray box hanging just under the angled blast defector. A
spark from this transformer is used to ignite the motor. The launch pad
itself is made from regular plumbing pipes and associated elbows and
tees. The launch rod is held in place by a 1/2 inch drill chuck. |
 Photo by
Mary Nielsen |
This
is me
with my first Hypertek hybrid motor rocket. This is a stock built
PML Tempest kit that I first flew on May 11, 1996. This was the
first hybrid launched in Idaho. I used the small orifice for maximum
thrust duration. This is the J100 configuration. The ALTS-2
altimeter reported 4523 feet. Unfortunately, after many flights,
this rocket eventually crashed due to a torn shock cord on a less than
totally vertical flight. When I built a new one, I stretched it
about 10 inches. The stock Tempest kit is, in my opinion, a bit
short on room for the parachute and recovery harness. I also
switched to tubular nylon and threw away the elastic shock cord. |
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First hybrid launch in Idaho.
May 11, 1996
Peak altitude was 4523 feet. |
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The Tempest had many
successful flights but this is what you get when an elastic shock cord
eventually breaks!
Tubular nylon is
a much better choice for large rockets. |
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