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* Comparison of
approximate current loads with a strong 12V source, ignoring transient
effects for simplicity. MF typical resistance 0.8 ohm, ML typical resistance
1.0 ohm.
A strong 12V source can: More Flight Tests: Clusters and Deployments using Rocketflite MF Ematches At the 4/19/08 CMASS launch in Amesbury, MA:
Flight 1: the
TOGinator The MF ematches were set up in 8 strings of 3 MFs in series plus 1 string of 2 MFs in series. Confirmed resistance / continuity: 1) when making MF’s, 2) after assembling the series strings, and 3) again after inserting the MF’s in each engine and before connecting the 9 series strings of MFs in parallel. Every resistance check was good every time. Comparing ignition system current load, ignoring transient effects for simplicity: For this flight using MFs in series strings of 2 or 3, the total launch system load was about 48A. Using a typical igniter like the Rocketflite ML all in parallel, the total launch system load would be about 310A. Also used MF’s to fire the two ejection charges using a Perfectflite HA45K altimeter. The liftoff was dramatic, with the jets of flame spread wide, big cloud of smoke, and every engine firing! The rocket lifted off quickly due to the 160 lb thrust spike at the beginning of the 1.8 second engine burn, and reached an altitude of 765 ft. All 26 engines fired, as did both ejection charges.
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Making Rocketflite ML (Magnelite) igniters: Step 1: Dip ML wire into ML pyrogen. Making Rocketflite MF Step 1: Dip MF wire in MF pyrogen.
Step 3: Dip in MF sealant. Step 4: Let dry for one hour.
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All engines fired, sending the rocket soaring to 1676 ft on a cool looking rose colored flame with a white core, due to the red G’s and white F’s. Both ejection charges fired for good dual deployment recovery on a Top Flight Recovery 5 ft Crossfire chute.
MF ematches fired the
engines set up in 2 series strings of 2 MFs and 1 series string of 3 MFs,
and also fired the two ejection charges. The only difference in the preparation of the ematches for their different roles in these successful cluster flights, was that the MFs intended for BP engine ignition and ejection charges were dipped about 3/8" into the pyrogen (that is how long their heads were) and the MFs used to ignite AP 29mm engines were dipped about 5/8" (matching the head length of AT's igniters).
Rocketflite prototype
MF ematches made it possible to fire everything 100% successfully with one
type of ematch: Tests: Instant AP ignition Using AT 29mm G64W engines, I experimented with adding small pieces of Blue Thunder propellant, pressed BP, or Rocketflite ML pyrogen, successfully achieving near instant engine ignition with all three methods. For all these tests I lightly sanded the inside of the propellant slot first. With the BT, used a thin strip jammed inside the G64 propellant slot. Pressed BP was a 1/8” thick slice of a 13mm Estes engine core, placed inside the space above the propellant and below the delay. The Rocketflite ML pyrogen, about 2x what would go on an igniter, was placed inside the top of the propellant slot. First I evaluated the speed of ignition by attaching an LED light to the pad ignition circuit in parallel with the MF ematch and video recording the launches. By counting the video frames at 30 per second, I could see that all three methods had the G64’s up to pressure within 0.1 second. Without “extra help” a G64 typically comes up to pressure in 0.3 to 0.5 seconds.
Later I set up a 3 way and a 6 way drag race, with augmented AT 29mm G71R’s getting off the pad faster than BP powered saucers due to the raw power of the engines. Testing also revealed that BT located above the propellant was not effective, and that larger amounts of ML pyrogen were not necessary. The method I prefer to boost AP ignition speed is Rocketflite ML pyrogen, as that poses the least risk of over pressurizing the engine. Now I was ready to fire mixed engine types in clusters with confidence that all engines would be firing before the rocket started to rise up the launch rod. J and K Impulse Clusters
At NERRF 4 (6/20/08-6/21/08) used MF’s with
including: The Saturn V went up fast on a 5 engine K impulse cluster, with a Cesaroni K-445 and 4x G64's. Used a Rocketflite ML igniter for the center motor and MF igniters in the G64's. Worked like a charm, kicking all five engines instantly for a hard long thrust to 3,372 ft. Total impulse 2095 Ns. The Ultimate FireBall went up on a J powered cluster of 7x RoadRunner G80-10’s, ignited by MF's. Fast smoky liftoff to 2462 ft.
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2008 Flight / Engine / Ejection charge countfired by Rocketflite 26awg MF prototype ematches |
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|
TOGinator |
VooDoo Daddy |
Ultimate FireBall |
Others |
Total |
|
Flights |
2 |
3 |
3 |
27 |
35 |
|
AP Engines installed |
3 |
- |
21 |
25 |
49 |
|
BP Engines installed |
53 |
28* |
- |
22 |
103* |
|
Ejection charges |
4 |
1 |
6 |
4 |
15 |
|
Total MFs installed |
60 |
25 |
27 |
51 |
163 |
|
* Four second stage engines were ignited by first stage engines |
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2008 flying season
results using prototype Rocketflite 26awg MF ematches:
> Ejection charges: 15 attempts / 15 successful
> 148 engine ignition attempts, of these:
* 142 fired on the first attempt
* 3 had clay covering the BP in the nozzle and were fired later after this
was removed
* 1 was an old stubborn F21W, which confirms that a hard to light engine
likes a long firing igniter
* 2 were engines in good condition that did not fire due to apparent failure
of the MF ematch
Engine ignitions (BP and AP): 144 attempts with engines in good condition /
142 successes.
Bottom line, Rocketflite prototype MF ematches provided 99% reliability in
the field.
The MF ematches achieved this performance while requiring much less current
than typical igniters.
2008 lessons learned firing MF ematches
A single MF can be fired by one AA alkaline 1.5 volt battery, allowing the most basic launch system to fire anything up to a 29mm AP engine.
Small clusters of MF’s may be fired by 6V to 9V ignition systems. Ground testing an ignition system is a good idea prior to flying clusters.
Large clusters should be fired by a strong 12V ignition system with a relay.
Disclaimer
Please note that I do
not speak for or represent Rocketflite. Rocketflite has sent me
supplies for tests.
What I have written describes my tests and projects as
an individual rocketeer.
Please see
www.rocketflite.com for more information.