We successfully launched Launch Vehicle 2.3 (LV2.3) this weekend in Brothers, Oregon, at the Oregon Rocketry's Brothers Launch Site.
Launch information
Estimate elevation of hill by launch tower: 4900 ft MSL
Launch control was at (GPS): 43 deg 47 min 55.4 sec 120 deg 38 min 54.5 sec @ 4459 ft
Launch tower was at (GPS): 43 deg 47.652 min 120 deg 39.0889 min @ 4488 ft (2m accuracy w/10 satellites)
Drogue was 16 paces and main was 34 paces away from LT, and between them was 32. Tim's paces are ~ 6 ft.
Saturday morning drive and afternoon setup
We gathered at Tim's house Saturday morning at 9:00am to pack all of our rocket bits: launch tower, antennas, launch control table, etc. We managed to pack it all into the back of Dave's pickup truck and in Dan's brother Bill's "Toy Hauler" - a large 5th wheel ATV carrier (thanks Dan! thanks Bill!). It was pretty amazing, actually: it was probably the fastest packing and smallest number of vehicles carrying rocket bits we've ever had since LV0. And, amazingly, we actually left on time.
We arrived in Brothers around 5:00pm, and in the last few hours of sunlight, managed to raise the launch tower and set up the antennas.
Done with setup
Saturday evening sunset
Thunderstorms to the west
Saturday evening we stayed up late carefully prepping the avionics module and Dan's helicopter... but we - shockingly- even managed to get some sleep.
This was an "airframe only" launch, but we still managed to cram in a bunch of systems into the rocket:
An Ozark Aerospace ARTS flight computer (hooked to the nose separation ring and the main chute line cutter
a 2m backup system, which used a Alinco DJ-7T 2m radio hooked into a Atmel ATMega168 with a DTMF decode chip (also hooked to the NSR and 2nd line cutter).
Keith's Telemetrum flight computer, with GPS (flown as payload only, with it's 900 MHz telemetry sending real-time telemetry and acting as a direction finder).
An Olimex LPC2148 development board with SCP1000, MP3, and ADXS pressure sensors and ADXL3xx 2 axis accelerometer.
Dave and payload
Andrew working on payload
working late into the night
Dan working on his helicopter
Sunday morning prep
Sunday morning we got back to work 9:00am, did a final checkover of the avionics, attached the igniters, buttoned up the rocket, and took it to the launch tower.
Rocket Cam
Launch Tower Computer
Prepping the launch tower
Putting together the rocket (avionics through motor bay)
We were ready to go by about 12:45pm, just in time the 12:30pm - 2:30pm waiver that Jeff of BORG called in for us. Again, surprisingly, we were ready to go, we just had to wait for a cloud break. After waiting about 30 minutes for a largish patch of blue sky, we turned on the avionics system(s), and cleared the pad.
Pete loading the N motor
Ready to go
Rocket and launch tower
One fun distraction was Dan's electric "T-Rex" helicopter. He strapped our spare camera and 2.4 GHz ATV transmitter to the nose and buzzed launch control and the launch tower. We had high hopes to catch the launch from the helicopter's perspective, but a loss of RC control made the 'copter crash and snap a blade. Next time!
Helicopter pre-flight
Helicopter on its way!
RC Helicopter flight movie (14 MB)
Sunday afternoon launch.
Ian hit the "launch" button at about 1340 PDT in our Java "LaunchControl" software that he patched for this airframe-only flight, and it counted down and launched the rocket over the WiFi link to the launch tower. The rocket leaped off the pad on Pete Ekstrom's "N" motor with a eery blue glow. We heard two large reports, which later we figured out was the motor "chuffing" (overpressuring).
We lost track of the rocket as it went above the cloud layer, and we all desperately were hoping the parachute system would work. Keith lost telemetry for a a few seconds, but once he got it back, he was able to announce that we were falling slowly enough that we should be on the drogue.
Looking for chutes!
And indeed, about a minute after that, the drogue and rocket were sighted.
LV2.3 falling on the drogue
Rare shot of the main deploying
Nosecone and main body
Finally, the ARTS board fired the line cutters and the main chute came out. To top it all off, the rocket landed only a few hundred feet from the launch tower!
Nose cone and drogue parachute on ground
rocket body and main parachute on ground
A well used motor
And just in time, too: about an hour after the launch, the winds whipped up and started blowing over tents and people, and it started to drizzle. We packed up in record time, and headed back to Portland.
All in all, a perfect flight!
Thank you to Jeff and BORG for arranging the waiver.
Giant thank yous to Liz, Casey and Alex for helping out so much.
TODO: Post graphs and final altitude and velocity numbers.
Data Analysis
High Speed Video
Using the calibration board behind the launching rocket and the high speed camera we are able to extract high quality data from the first few moments of flight.
Using the open source video analysis tool Tracker we are able to estimate the altitude, velocity, and acceleration of the rocket over the first 0.3 seconds of flight.
Using Tracker:
The large black and white blocks of the calibration board are 30 cm in height. A calibration stick is used to set the size of pixels in the video. Then the position of the rocket is tracked with the subpixel tracking feature in Tracker. The axis is set such that the motion of the rocket is assumed to be entirely vertical.
Altitude
Data from the fight speed video shows a smooth take off.
Velocity
Some noise seeps into the data now, but smooth acceleration is shown here.
Acceleration
The rocket comes up to about 10 g's almost immediately. Because of the double differentiation and the quantization noise in the image, the acceleration graph is very noisy, this one has been smoothed heavily.
Notes on the launch
We need straighter fins
better fin clamps? Screw holes so close together may torque fins?
Bar between clamps and fins? Could use shims between clamp and bar.
2m backup system
horizontal polarization of the bird feeder didn't reach the rocket on the rail (again)
Better long wire antenna?
Arm rocket by local HT at pad,
or multiple (diverse) 2m uplink antennas
Goal: verify 2m operation in flight.
Here's the hand drawn schematic of the 2m backup system.
We must know you are coming ahead of time (email 'info' at 'psas.pdx.edu'), and attendees must sign both a PSU and Tripoli Rocketry Association liability waiver.
Possible showers on Saturday, partly sunny on Sunday. It'll be ~ 60-70 during the day, but it's going to get awfully chilly at night. Here's the weather forcast.
Transportation
People, cars and stuff leaving Saturday morning
Who
In What
Other people?
With What
Andrew
red van
1, maybe 2
tools, pop-up tents, etc., 2nd Yeasu for backup
Dan
truck?
?
"Toy hauler", tools, rocket.
Dave
truck
Candace, 3-4 other people
Dan's trailer, with launch tower and other large things, and tools.