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Day 110 - Polaron G2 phase 2 development
Getting ready for the static thrust tests.
The G2 main stage is attached to the test
stand. Due to it's length, it is attached to the
balcony.
The yellow string stops the rocket swinging
sideways during release. The black string stops
the release head from hitting the ground.
Top of the main stage connected to the load
cell.
9mm nozzle under test.
Another test. The bricks stop the spray from
coming back towards us.
Making booster parachutes.
Finished parachutes.
Lower spliced quads
Date:7th
August 2011
Location:Workshop, Australia
Conditions:Mild, rainy
Team Members at Event:PK and
GK
Polaron G2 - Phase 2
This week we have been focusing on the phase 2 development of this rocket. Phase 2
is basically the addition of boosters to the
main stage, and switching the main stage to
the Jet Foaming configuration. This also
involves upgrading the cluster launcher to
handle the greater loads.
Main Stage - Jet Foaming static tests
This weekend we ran a number of static
tests on the main stage to measure the
amount of thrust generated and the thrust
duration.
We removed the fins and the nosecone from
the G2 rocket and added a reinforced spliced
pair of bottles to the bottom of the stack.
This added another 3L or so to the overall
capacity. We also used the same Jet Foaming
spacer as we trialled on the Axion G2
rocket. For these tests we just used a
standard 9mm Gardena nozzle on the main
stage. This nozzle would normally be too
small for a rocket this size, however, with
the higher pressure and the boost in
velocity on launch, it is fairly close to
where we want to be. We want a nice long
burn from this rocket.
Because of the length of the rocket we
had to suspend our normal test stand from
the balcony.
On Saturday we ran a couple of tests with
4L of water + foam at 205psi. The tests went
well except when we sat down to review the
thrust curves we realized we didn't quite
have the load cell amplifier turned on
(*Doh!*)and so we captured a little bit of
noise. The tests at least allowed us to
measure the thrust duration.
So on Sunday we repeated the experiment
and re-ran the two tests at 200psi with the
load cell amplifier turned on this time.
Although the rocket will use higher pressure
for actual flights we decided to use a lower
pressure to reduce the risk of an explosion
in our back yard.
We captured good data from the Sunday
tests.
Test
Pressure
Thrust
duration
Water
Amount
Total Impulse
1
205 psi (14.1 bar)
11.2 s
4L +
foam
N/A
2
205 psi (14.1 bar)
10.6 s
4L + foam
N/A
3
200 psi (13.8 bar)
11.4 s
4L + foam
218 Ns
4
200 psi (13.8 bar)
10.2 s
4L + foam
227 Ns
Here are the two raw thrust curves from
test #3 and #4:
The thrust curve is interesting because
after about 1.2 seconds you can see the
thrust increase as the pressure drops
which is a little strange but when we
subtract the weight of water as a function
of time we see the thrust curves are more
like this:
Note the rate of water loss in only an
estimate since we can't accurately measure
it. The increase in thrust becomes less
dramatic, although it's still present.
The dip in the thrust curve around
1.2 seconds is the result of water running
out in the bottom bottle. The 8mm nozzle
inside the jet foaming spacer limits the
rate at which water can enter the lower
bottle, but the 9mm nozzle being bigger can
empty the lower bottle faster.
The raw thrust curve is actually the
one we are interested in because that is the
effective thrust causing the rocket to
accelerate upwards since it already
incorporates the weight of the water.
Here is a short
video of the static tests:
From the tests it looks like we should
get a nice long foam trail! :) The interesting
thrust curve makes me think it may be
possible to customize a thrust curve shape
to a certain extent with a series of baffles
in the pressure chamber with different sized
holes and varying amounts of water/foam
above each baffle.
Other Development
Boosters
The lower spliced-quad of each
booster is now reinforced, but still
needs to be pressure tested.
We are using the Acceleron V nozzles
for each booster since they are already
done. These are 15.6mm in diameter.
We made up three new booster parachutes,
each is 700mm in diameter and weighs
27grams.
We are in the process of adding the
deployment mechanism to each booster but
they will be based on
this
technique like we used last time.
Launcher Upgrades
We need to strengthen the base of the
cluster launcher as at 250psi each booster
is going to be exerting about 320N on each
nozzle seat the equivalent of about 32Kg.
The release head also needs to be reinforced
as it will have about 1000N trying to rip it
out of the launcher. There will be a lot of
stress on the Gardena nozzle and it will
need to be made of aluminium again.
The stability of the entire launcher
needs to be improved because the rocket is
very tall, and could easily tip over as it
is.
A new narrower and longer guide rail
will need to be fitted.
One of the things we need to investigate
is how much we need to strengthen the neck
and throat of the lowest bottle to handle
the static force while on the pad with all
three boosters trying to rip it out of the
launcher.