Level 4 Certification
project - Circus4
|
Event |
Blazing-Archers 2002 |
|
Location |
Mountainview, Ontario |
|
Date |
September 1st & 2nd, 2002 |
|
Rocket |
Circus4, 5.54 inches in diameter
x 110.5 inches long |
|
Motor |
Hypertek 2800-300-MFX (M960) 5126 N/s |
|
Flyer |
Pierre Laurendeau CAR #S-301 |
|
L4CC |
Marc Ouellette (on location) and Dave Ross |
|
RSO |
Bill Wagstaff |
The Circus4 is a heavily modified
LOC Minie-Magg stretched to 110 ½ inches long, with three
LOC Magnum fins. The fins are through-the-wall / through-the-motor
mount with PVC ¾ inch molding used as reinforcements along
the fin roots to provide more surface area where the structural
strength isn't provided by Epoxy alone. The booster section is
designed to accept an M1010 Armageddon motor from Hypertek. The
Booster is reinforced with 6 centering rings which are joined
together using wooden rods that are glued together using epoxy
throughout the assembly. The rods and rings are all in contact
and glued to the fuselage forming a uniform whole. In addition,
three threaded 50 inch long metal rods were added before the
final build to add strength to the motor mount assembly.
This rocket was NOT reinforced
with fiberglass due to it's heavy-duty construction using internal
reinforcements instead of external reinforcements. The rocket
is covered with Hammerite paint mixed with fiberglass to give
it some extra external strenght, but this was done mainly to
make the overall rocket more resistant to the usual wear &
tear. The rocket has flown successfully on a Hypertek L550 and
landed safely on asphalt tarmac without a scratch
Some of my notable level 3
experience
PML Black Brant X, Flown with an Aerotech J motor
Illudium Pu35 Space Modulator, 6 inch diam x 66 inch rocket
flown on a Hypertek K hybrid motor
Bowling Ball Lofter, Flown with an Aerotech K motor
Circus3, Flown with a Hypertek L motor (Hybrid)
The motor I will use is a Hybrid
Hypertek M960 which is recognized and tested by Tripoli but who'se
technical specifications haven't been annonced yet. I have contacted
Cesaroni to obtain more details about the motor. The power of
the motor is 5126 N/s which is 6 N/s more than the absolute minimum
required for an M motor so this is clearly a baby M. The launch
site for the Mountainview launch will be sufficient for this
motor.
Electronics
The rocket will be flown using two Olsen FCP-M2 altimeters with
independant power sources. Each altimeter will fire independant
ejection charges. They are mounted in a 10 inch long standard
electronics bay reinforced with two threaded rods for extra strength.
Parachutes
The rocket will be flown with dual stage deployment using a 36''
drogue at apogee and two main 60 inch chutes fired at 1000 feet
(800 feet for the backup altimeter).
Flight Profile
Max Altitude : 2.29 Km AGL (2290 meters).
Max Velocity : 768 km/hr.
Rod Velocity : 100 Km/h at the end of the ramp .5 sec including
the oxygen burst.
Max Acceleration : 67 m/sec2 (6.7 G's roughly)
Flight duration : 120 seconds |