In particular, does a Telemetrum transmitting on 70 cm. interfere with a Perfectflite Stratologger SL-100? Anyone have any experience?
Also saw a video about a "lightning bug" dual-deploy altimeter (https://www.youtube.com/watch?v=IroVZC5ZbF4&t=10s) that uses a step-up transformer to produce an arc that lights charges without e-matches. Interesting, but I wonder how well that would work with a Telemetrum in the same rocket.
(My apology. This was initially sent in html and "scrubbed". Trying
again...)
Howdy, all;
I'm experimenting with some reinforced 3d printed recessed charge well
av-bay end caps for a Wildman Mach 2. I'm trying to understand the
actual forces encountered by the av-bay hardware during deployment, i.e.
actual v.s. simulated.
I typically fly with chute configurations where the rocket is descending
under drogue at around 70 fps and is slowed very quickly at main
deployment to around 16 - 20 fps. Within simulation, this results in a
25 G deceleration over a very short period of time, i.e. a deceleration
"spike". In reality, the main chute takes more than 0 seconds to deploy
so that the actual deceleration encountered may be significantly less
or, let's say, lower magnitude spread out over a long time.
In designing these end caps, finite element analysis shows that they
have tolerable deflection and should survive without any problems.
However, FEA on a 3d printed object is somewhat misleading as most FEA
assumes the material is homogeneous, for example machined from a solid
block of PET. When 3d printed, various effects yield a somewhat
heterogeneous material due to extrusion imperfections, inclusion of air
at the layer interfaces, and less than perfect cohesion between the
layers. This reduces the overall strength of the material and can affect
just how brittle it is as well, but just "how much" for a given object
is unknown.
I'm slowly working up some prototypes and have created a rig where
static and dynamic "drop" tests with a representative mass can achieve
loads similar to deployment on the av-bay internal structure and its end
caps.
I'll be flying with a TeleMega and have had great success with these in
larger rockets with "conventional" av-bay end caps. So, while this is a
bit off topic, I'm hoping the community may be willing to share some
simulations and flight data for similar rockets.
For example, if you have and are willing to share BOTH a simulation
model (and simulations) in either Rocksim or OpenRocket AND
accelerometer data from a rocket with similar flight characteristics,
that could be especially useful to me. I'm hoping to see 1) what
deceleration is indicated under simulation for the drogue to main
transition and 2) how close is that to what was actually logged by an
AltusMetrum product (.eeprom file). Yes, I realize that because the data
is sampled, the system and resulting eeprom file may not contain the
instant of maximum deceleration actually encountered by the airframe.
However, I can learn a lot just by observing the shape and extents of
the deceleration curve.
That would allow me to get some confidence in whether my drop tests are
actually similar to what's experienced in flight, or not, and would
drive the design and build to completion (or abandonment).
Again, I'm looking for information on rockets / flights with the
following characteristics:
Total mass around the range of 57 oz (w/ H283ST) to 122 oz (w/ K375NW)
Descent under drogue around 70 fps
Descent under main around 16 - 20 fps
Since this is all about deployment loads, your rocket doesn't have to be
as fast or go as high as a Mach 2. In fact, if there are both simulation
AND flight data, just about anything close will work as I'm mostly
interested in the difference between simulation and reality. I expect
both "much larger" and "much smaller" rockets have other factors, like
body drag, etc., which will make the comparison less relevant so I'm
hoping to find something similar in size / mass to the Mach 2.
Anyway, if you're able to help, I'd appreciate it! I don't know how
interested the list is in this topic so it's your call as to whether you
reply direct or via list. Either way, thank you, all, in advance.
Clear Skies,
Dave Andreatta
TRA #19131
WD0HXN
Erie, CO
A brand new TeleGPS I just got (SN 7445) does not save any data. There is only a single ~3 second “flight" out of some back yard near Colorado Springs. I thought it could have been user error the first time I flew it, but it just went up for the second time with the same results. Also, right after launch it says “GPS lost” and there is no telemetry for several seconds, and then it picks up the flight, but the TeleGPS program reports a new starting altitude so the altitude and apogee on the Status screen are way off. The location and maps work. The most recent files are attached. Any ideas on this one? Some way to configure or fix it locally? Or does it need to be sent in?
Charlie
Hi Bdale,
I'd like to register our HPR launch site in Illinois:
Fox Valley Rocketeers (FVR); 042deg 19 min 42 sec N, 088deg 31min 35 sec W;
http://FoxValleyRocketeers.org
Thanks!
Ed Chess
I'm trying to build AltOs on my pinebook pro (ARM laptop) and running
into some difficulties. Seems like AltOs, despite being written in
java, has some compiled libraries so I can't use the prebuilt binary
release.
I keep getting hung up on a step that seems to be making icons:
nickle led.5c redoff.png
Cannot autoimport from file "cairo.5c", giving up.
Cannot autoimport from file "cairo.5c", giving up.
import Cairo;
import Cairo;
:1: non-existant namespace Cairo
led.5c:21: syntax error before "cr"
led.5c:38: syntax error before "led"
:1: non-existant namespace Cairo
led.5c:40: syntax error before "::"
led.5c:41: syntax error before "::"
led.5c:42: syntax error before "::"
-> set_source (cr, led);
led.5c:43: No visible symbol "set_source" in scope
-> set_source (cr, led);
led.5c:43: No visible symbol "cr" in scope
....
There are a bunch more similar errors but they seem to be similar.
My googling on these errors hasn't been super helpful. How can I fix
these errors?
Thanks,
Jesse
Getting ready for the spring flying season and updated Altos Droid to the
latest version. Now the app crashes immediately upon opening?
"Unfortunately, Altos Droid has stopped." is the only error i get.
Tablet is a Samsung Galaxy Tab A (2016) The Android version is 5.1.1. I
tried a factory reset and reinstalled AD but no change. Other than the
update I'm not aware of any other changes to the device and Altos Droid
used to run flawlessly prior to the update.
Anyone have any suggestions?
Andy Barwick