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(Click on photos for an enlargement.)
This project started because I wanted to do something
different. I had been doing camera rockets exclusively for over 12 years and wanted a
different challenge. When I considered an upscale of a model rocket, I knew the only
choice for me was the Mars Snooper II (Photo 1). It was first released by Estes in 1975
and ran through 1980. Because of its futuristic design I thought it would be a challenge
and an attention getter. It proved to be both.
I had a Mars Snooper II a long time ago but I never cared
for its paint scheme. The original was painted almost entirely red with only white decals.
I painted mine red but I added black for the fins, reducers and nose cone. For the upscale
I wanted a multiple color scheme so I opted for a white body tube with black fins and
reducers and then trimmed with silver and red (Photo 2). Also it is not a true upscale
because of the cooling fins. The original had only 8 and I wanted nine for symmetry.
I decided to make mine out of fiberglass. The 4 times
upscale showed that it would be 8 feet tall (Photo 3) and the fin span would be about 3
feet, and I knew I needed something substantial to withstand the forces of flight. I
designed it around a 75 mm motor mount so it could be capable of (theoretically) Level 3
flights. Because of these differences I decided to call mine the Mars Snooper III.
The first challenge was the general design of the rocket.
With a 75 mm motor mount there wasn't enough room in the 4 inch body tube for both the
longer motor and a parachute. The parachute would have to go into the upper 3 inch body
tube. How would they be connected to get the parachute attached to the lower section and
still have access to install the electronics for ejection? I designed the motor mount tube
to go all the way up to the top of the 4 inch tube and use a long coupler that the 3 inch
upper section would slide over. The coupler would have to be long enough for screws to be
installed above the upper transition. These screws would prevent the upper body tube from
coming off at ejection. The electronics would be installed via a hole in the coupler and
then slid down into the 4 inch body tube and attached.
Photo 4 shows the motor mount with the fins before the 4
inch body tube is installed. The motor mount extends to the top to the outer body tube and
the coupler extends 12 inches beyond it for the upper body tube to attach. The opening in
the coupler tube allows the electronics to be installed and the lower opening is so it can
be placed next to the outer 4 inch body tube. This allows the outer body tube to be free
from a door to access the electronics.
The design also proved to be a challenge because I knew the
fins had to be attached to the motor mount very well. The fins would be heavy and the
acceleration could easily rip them off if they were not attached well. The shock when the
rocket landed would be even greater. The fins were constructed from 1/8 inch G-10
fiberglass laminated with 3/16 inch plywood. The entire thickness would be a true scale
1/2 thick. For the fins outside the pods (Photo 5), I used slightly thinner 1/8 inch
plywood so they are only 3/8 inch thick as well as the upper fins.
To help absorb the shock on landing I decided to have
retractable legs that were spring loaded. This was accomplished by attaching the fins to
an inner 1 1/2 inch fiberglass tube. This inner tube would house the spring for the legs.
The 2 1/4 inch tube would surround this inner tube to give the pods a through the wall fin
mount (Photo 6). The pod nose cones (Photo 7) were turned from stock nylon by my father
and would be glued on after a 1/2 inch brass tubing was epoxied inside to guide the leg as
it retracted (Photo 8). The nose cone had to be hollowed to allow the leg to travel inside
from the 2 inch compression of the spring. Each fin weighed about 4 pounds without the
leg.
The fins were attached one at a time using a jig to hold
each leg in place until all could be securely fastened (Photo 9). Attaching each fin was a
several step process. Each fin was tacked in placed with slow CA. Then carbon fiber was
used to run the length of the fin and covered with more CA. A thin layer of 5 minute epoxy
coated the first layer of carbon fiber to hold each fin strong enough to rotate the rocket
and attach another fin.


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Photo 10
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Photo 11
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Photo 12
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Photo 13
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Photo 14
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Photo 15
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The next layer of carbon fiber was attached in short
lengths so the grain of the carbon was perpendicular to the root edge (Photo 10). It was
again glued with CA and a third layer of carbon fiber covered the second, running the
length of the root edge (Photo 11). The entire joint was flooded with 2 hour epoxy. The
upper end was sealed by the centering ring, also re-enforced with carbon fiber, and the
lower end was dammed with red modelers clay (Photo 12). This was just the joint at the
motor mount.
The 4 inch body tube was slid over and tacked in place.
Carbon fiber was used with CA over the length of the fins and lightly coated with 5 minute
epoxy. The inside joint was also coated with a layer of carbon fiber and completely soaked
with 2 hour epoxy (Photo 13). Because the lower part of the fin would be covered with one
of the transitions I could also build up the fin underneath the cowling.
Small strips of wood were glued to the fins where the
transition would be attached to the fins to give some support for the cowling and the
centering ring for the cowling was attached to the base of the body tube. Cross weaved
carbon fiber was attached between the fin, the body tube, and the centering ring. Then
another deep cure of 2 hour epoxy (Photo 14) was used to soak the carbon fibers.
The upper fins were attached in a similar fashion. They
also had through the wall fin construction and even the 3 inch inner tube was slotted. The
coupler to hold the upper parachute compartment extended down below the upper fins and
provided additional support. The joints were also re-enforced with carbon fiber and inner
fillets were also used (Photo 15).
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Photo 16
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Photo 17
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Photo 18
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Photo 21
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Three transitions had to be made, the upper transition for
the 3 inch body tube to the 4 inch body tube, a transition at the 4 inch body tube at the
fins, and the lower reducer acting like the motor with "cooling fins". All were
cut out of poster board and then coated with three layers of 6 ounce fine weave fiberglass
and 2 hour epoxy. The upper and lower transitions could be built "in place"
attaching the paper directly to the body tube and centering ring (Photo 16). The
transition at the fins could not because of the through the wall construction. It was
placed temporarily on a jig and covered with the fiberglass and epoxy (Photo 17). When
dried it was cut for the fin slots and then sliced and installed on the rocket. The
"engine" reducer had nine "cooling fins" made from 3/32 inch
fiberglass and attached with the standard CA, carbon fiber, and epoxy joint (Photo 18).
All the transitions were filled with expanding foam to give them rigidity.
How was the rocket going to be guided at takeoff? The
original rocket used two launch lugs attached to both sets of fins set far enough from the
body tube to allow the rod to clear the transitions. That would never work for this
rocket. I decided to still use a 1/2 inch launch lug but attached directly to the 4 inch
body tube that passed through the transitions. This also proved to be a challenge. I used
two sections of PVC pipe, one for each transition and then aligned them up with a standard
launch lug (Photo 19). The two transitions were epoxied together sandwiching layers of
carbon fiber. The launch lug fit nicely inside the PVC pipe and was used to align the two
pieces together.


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Photo 19
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Photo 20
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Photo 22
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The legs were constructed from solid 1/2 inch aluminum and
the feet were made from black plastic pipe that I found in the hardware store that fit
just beautifully over the legs. The legs were machined by my father with a groove to allow
a snap ring to hold a washer that would push up on the spring. They were kept from falling
out by a 1/8 inch aluminum plate that was attached to the bottom of the pods. In between
the two tubes of the pod were 6-32 standoffs (Photo 20) that the plates would be screwed
into.
The Center of Pressure was calculated and it is located
about an inch below the top of the main fins. I knew that nose weight would have to be
added for stability. Five pounds of lead shot were epoxied into the fiberglass nose cone
that surrounded a 5/16th inch piece of all thread (Photo 21). The all thread is used to
attach the parachute to the nose cone via a closed eye bolt.
The rocket was nearly finished except for a few touch ups
for the Turkey Shoot 2000 launch but I came down with the flu and just couldn't complete
it. Springfest 2001 came around and I was determined to fly it. Several people commented
on the looks and I started to get nervous. Am I really going to fly this rocket (Photo
22)?
With an empty weight of nearly 25 pounds, I knew I would
need a big chute. I ordered the 15 foot military surplus chute and at the launch field it
was quickly apparent that it would never work. I managed to get it into the rocket but I
knew that it would never deploy. Fortunately Dave Flynn volunteered a Rocketman R9C and I
had a R7C that could be used for the nose cone. The L850 was assembled and the ALTACC
installed and it was ready to fly.
I used my custom launch pad that consisted of basically a
table with a hole in it and a launch rod. Its a great design because the weight of
the rocket sits on the table rather that the hanging off the rod. The launch rod is used
entirely for guidance rather than supporting weight (Photo 23). Even still I heard cracks
about serving tea out in the launch area (sigh). The table was staked down to prevent
tipping over and the igniter installed.
The winds were too strong most of the day but had been
dying down. The nervousness was turning into butterflies, launching a very unusual design
that weighed about 35 pounds at takeoff from a 6 foot 1/2 inch launch rod. It was stable
but the design still made it risky in a wind. The simulations had it stable in flight at
about 40 inches and it did have an 8 to 1 thrust to weight ratio. To top it off, I was
using too small of a chute for the booster. Hit the button anyway.
The launch was perfect (Photo 24). It climbed straight and
seemed to continue for a long time (Photo 25). Very little weather cocking was evident and
right at apogee the rocket separated. The nose cone chute opened right away but I wasn't
breathing until I saw the booster chute. After an eternity passed without breathing I saw
the booster chute opened (Photo 26).
I saw both chutes out but knew that the chute for the
booster was too small. It was designed for a 15 pound rocket and the booster had to weigh
at least 22 pounds. What was I thinking! It landed and the spring loaded legs helped
cushion the impact but all three legs bent upon hitting that hard dry lake bed (Photo 27).
One of the reasons that I wanted removable legs was that if they were damaged on landing,
they could easily be replaced. Dave says that I should use stronger springs and aluminum
for the legs. I'll probably do that if I ever fly it again.
Other than the legs there was only cosmetic damage where
the outer fin had attached to the pod. This was probably caused more by tipping over than
the actual impact on landing. Nowhere the main fins attached to the rockets body were
there any signs of cracking. The tedious re-enforcing had paid off.
Overall the Mars Snooper III provided me with valuable
experience and a whole host of emotions. Everything from loving it to wanting it off my
workbench because I was sick of the sight of it. Will it fly again? Perhaps not. I like
the design of it so much I'm considering just using for a conversation piece and taking it
to science fairs and such to promote HPR. |