The RRS was glad to have another launch event at our Mojave Test Area (MTA) on Saturday, July 13th. Our event this time was with Operation Progress in Watts. Thanks to our partnership with the LAPD CSP, we are able to fly nine alphas and a beta rocket at this event. It was to be a typically hot July day in the Mojave, but the winds were still through the morning picking up a little as the afternoon went on.
This was my first time as the event pyro-op. New member, Kent Schwitkis of Compton College and Waldo Stakes assisted me with the operations as we gave our young rocketeers a great view of their hard work.
As the LAPD CSP arrived at the RRS MTA, the society prepared to give a site tour to the students followed by our safety briefing.
Our sample propellant burn demonstration gave the students a visual indication of what would be to come with the propellant driving their custom painted rockets into the blue sky. With the briefing and demonstrations complete, the students took shelter in the observation bunker.
One of the interesting features I noticed with this set of alphas was the use of modelling clay at the nozzle to hold back the micrograin propellant. This proved to be an equally effective method of holding back the propellant when the rocket is in firing position as the typical phenolic thin disks we commonly use.
One of the alpha rockets was outfitted with a whistle on one of its fin. Although imparting a spin during flight, the alphas tend to remain somewhat stable in flight. The results from this flight was somewhat disappointing as the whistle could not be clearly heard in either ascent or descent before impact.
Our last rocket for Compton College was the larger RRS standard beta rocket. This two-inch diameter powerful vehicle made its impressive mark on the launch pad as it tore into the sky. After the launch, we took break for lunch. With the day growing hotter by the hour, our partners with the LAPD CSP and Operation Progress bid the MTA and the RRS farewell as they returned to the city.
Following lunch, our second group at the event was a team from Compton College made up of Prof. Kent Schwitkis and Brian Johnson and their students. The Compton Comet was a standard alpha rocket outfitted with an instrumentation package and a parachute.
New RRS member, Professor Kent Schwitkis got his first experience with loading the micrograin propellant in the Compton Comet at our loading area. This is a rite of passage for many of our new members. Although old and grossly inefficient, the zinc and sulfur powder propellant combination offers a simple and powerful combination to lift rockets in a yellow rushing plume.
The Compton Comet was loaded by the team into the alpha launch rails. All of us retreated to the concrete bunker for firing.
The Compton Comet parachute somehow failed to deploy. The ballistic return of the rocket meant extraction by the time-honored method of shoveling. The Compton College team showed tremendous fortitude in the scorching 110 degree weather. The fruits of their labor was the return of the instrumented payload including the data chip inside.
Initial results showed that data was taken throughout the flight. The results are being reviewed by Compton College to be reported later to the society.
This was a very successful launch day at the RRS MTA and the society was glad to support the Operation Progress and Compton College student teams at our Mojave Test Area. For more information on similar rocket building programs with the RRS, contact our events coordinator, Larry Hoffing.
For all inquiries about using the RRS MTA, contact the RRS president, Osvaldo Tarditti
The RRS was glad to host an event at the Mojave Test Area for the UCLA Rocketry Club. This group of two dozen students launched a series of G-sized model rockets for their rocket building event on July 10, 2019.
Each of the rockets had an egg as its payload. All but one was recovered intact. Each rocket had a custom data logging package including a barometer as an altimeter and an accelerometer. Average altitude was 2,480 feet with a group average peak acceleration of 14 G’s and thrust of 25 lbf.
One concern some of our members had from last week was if any of the structures at the MTA suffered any damage from the recent pair of earthquakes at Ridgecrest only a little more than 30 miles away across the dry lake desert floor. The RRS is happy to report that the damage seems minimal in that both the old block house is still standing and the George Dosa Building doesn’t look any worse for wear.
The RRS was glad to support this student event with UCLA. There will be a second, similar rocket building program later this month. For questions about future events, contact Larry Hoffing
It was the Saturday of Memorial Day weekend. My flight was experiencing rough turbulence as it flew over the mountains on final approach to El Paso, TX. I was traveling to Spaceport America as a sponsor on four upcoming space-shot attempts. After collecting my luggage, I picked up my rental truck and headed north on the two-hour drive to Spaceport America. The only other way to access Spaceport America is to fly into Albuquerque and make the three-hour drive south. I had decided to fly into El Paso to save some time. Texas had actually been my home ten years earlier while working at NASA’s Johnson Space Center as an International Space Station (ISS) flight controller.
Getting through security earlier that day had been an adventure. My carry-on only contained mission critical hardware and was flagged for inspection. Everyone in the security line stared as TSA agents pulled antennas, circuit boards, a soldering iron, hot air rework station, trays of SMT (surface mount) components, wiring, ground control units, and weather balloon inflation equipment out of my carry-on. Everything was thoroughly swabbed for explosive residue and a lot of questions were asked.
The reason I had been asked to sponsor the next four launches at Spaceport America was because I had led the development of a new set of avionics for professional rocketry. It consists of a flight computer called the Eagle and a handheld ground control station. It was developed as part of a program for safely launching and recovering rockoons. It has the ability to launch, stage, and recover a multi-stage rocket as well as other proprietary features unique to rockoon flight. It has a very accurate barometric sensor and an aviation-grade inertial measurement unit (IMU). However, what space-shot teams find especially appealing is the global positioning system (GPS) receiver that can obtain GPS lock at any altitude.
The first launch was set for Monday morning at
6:00 AM. The rocket was a two-stage rocket built by Coleman Merchant from
Princeton University as part of his master’s thesis.
It had the energy and propellant mass fraction to easily pierce the von Karman line (100 km of altitude). A group of cadets from West Point were also on site to assemble and align the launch rail on loan from Kevin Sagis, Virgin Orbit’s chief engineer. My responsibility, in addition to monitoring the health of the Eagle avionics package, was to launch weather balloons in the hours leading up to the rocket launch. This was critical for obtaining the upper level winds for calculating the firing solution. In the coming week, I would be launching a new type of radiosonde I had developed that would help lower the cost of obtaining upper level wind analysis prior to rocket flights.
At 3:30 AM Monday morning, the team assembled for final launch preparations. Radiosonde operations were going well. Preparations at the launch site were also progressing smoothly. However, there were concerns that the brackets used to bolt the 1010 launch rail to the main launch rail structure could make contact with the carbon fiber fins on the booster during launch. This hadn’t been apparent earlier since the launch rail was still being prepared the previous day. The decision was wisely made to delay the launch. An hour later, all the brackets had been trimmed using a hacksaw.
After aligning the launch rail with the final firing solution obtained from my radiosonde data, the rocket was armed. We all moved to Mission Control to complete final checks. This is when we discovered another technical issue. Since so many electronics, transmitting at various frequencies, were crammed into the nosecone, and since the nosecone was in such close proximity to the large launch rail structure, it was taking longer for the electronics to obtain GPS lock. We had done a radio-frequency (RF) test of the avionics package with all electronics running the previous day, including GPS lock testing, but not on the launch rail since it was still being assembled. It took about five minutes, but eventually all electronics with GPS receivers had GPS lock. After getting a “go” from White Sands and Spaceport America, the final countdown resumed and Chase Lewis, the West Point pyro-lead, sent the signal that launched Coleman’s rocket.
Even from a mile away, it was difficult for the eye to catch it as it accelerated off on its way to space. Acceleration during boost reached 46 g. At booster burnout, the rocket was traveling Mach 2.4. A charge fired which separated the sustainer from the booster. A few seconds later, the sustainer engine fired and the sustainer once again experienced a peak acceleration of 46 g along its X (vertical) axis. However, as speeds approached Mach 3.8, the rocket became unstable and began to fly in a large upward spiral. Acceleration on both the Y and Z axis, which should ideally be zero, hit 42 g. Somehow the rocket managed to hold together before exiting the earth’s atmosphere at which point all acceleration loads went to zero. A few minutes later, the rocket re-entered the earths’ atmosphere under drogue. The booster had landed much earlier. It didn’t have any electronics and its recovery method was ballistic.
After analyzing the data recorded by my avionics system (there were two altimeters by a different vendor but we couldn’t access the data), the leading theory for the upward spiral was inertial roll coupling. This is an aerodynamic phenomenon that can happen to both rockets and high-speed aircraft at a critical roll rate. Symptoms include divergence of angle of attack, large side-slip angle, and violent accelerations and loads. Air-frames with a low roll moment of inertia are particularly prone.
We still had one more launch window the following day. The decision was made to launch the second rocket and see if the problem repeated itself. No two rockets have the same roll rate due to tolerances in fin can and nozzle manufacturing processes. The hope was that the second stage would either stay below or above the critical roll rate during sustainer engine burn.
The launch window for Tuesday had also been scheduled from 6:00 to 10:00 AM. However, White Sands Missile Range informed us shortly before 6:00 AM that our launch window would close at 6:35 AM. This was unexpected and placed a lot of pressure on the team as we prepared the second rocket for launch. The rocket was armed just a few minutes before the launch window would close and we didn’t have time to allow the electronics to acquire GPS lock. The decision was made to launch with the hope GPS lock would be acquired during flight away from the interference caused by the launch rail. The booster once again flew flawlessly, but the sustainer never ignited. It coasted up to 19.7 km (64,600 ft) before coming back down under drogue. None of the electronics obtained GPS lock during the flight. The chance of us ever finding the sustainer and determining why its engine never ignited seemed unlikely. In the distance, we watched a missile soar into space over White Sands Missile Range. Now we knew why our launch window had been cut short.
I knew my avionics system had line-of-sight range, so in theory, as long and I could get my hand-held ground station high enough above the terrain, I would be able to receive telemetry. One idea I had was to mount my handheld ground unit to the top of the launch rail. We lowered the hydraulically-actuated launch rail and taped my ground control unit to the tip before raising it back up. The ground control unit was now sitting 40 feet above the desert. We lowered it a few minutes later and were disappointed to see that the ground controller had not logged any telemetry packets. This meant the rocket had to be in a gully or valley at a distance greater than a few miles. The next idea I had was to drive back and forth across Spaceport America along the expected flight path. I knew that if I came within a mile or two of Coleman’s rocket, I would receive packets and we could then locate the rocket. After driving for about an hour down some very rough roads, my ground controller started to log packets. An hour later we all hiked out to the sustainer which was lying in a valley. The sustainer was very close to where the booster had actually been targeted to impact as calculated by the upper wind analysis and firing angle solution.
On the drive back from the recovery area, I got a flat tire from an old fence-post nail. I tried to speed up through the cloud of dust from the truck in front of me to flag for help, but once my rim was hitting the ground I had to stop. I could have been out there for hours by myself if I hadn’t been able to break the lug nuts free with the inadequately short tire wrench I found under the truck’s passenger seat. Fortunately, I did make sure I had plenty of water, snacks, first aid kit etc., before heading out to try to find the sustainer.
So what went wrong on Coleman’s second space-shot attempt? It appears both altimeters rebooted when they fired the booster/sustainer separation charges. Because they were both rebooting, neither one fired the sustainer igniter. Since Coleman had only reached out to me two weeks earlier about integrating my avionics package into his rocket, my system hadn’t been approved by Spaceport America for initiating any flight events on his rocket. All it could do was go along for the ride while saving and transmitting flight data.
Coleman’s rockets had both flown amazingly well.
The first space shot had come amazingly close to space. You could tell that a
lot of experience and engineering analysis went into the design of his two
rockets. I asked Coleman what he enjoyed most about the project:
months, coming out with a really nice final product that you are really proud
of. Everything on this came out exactly the way I wanted it to. I don’t really
have any regrets about how it was made.”
They truly were both impressive rockets. I asked
Coleman what his biggest takeaway was:
time on the electronics than you think you should. Don’t leave it until the
last minute. It’s almost the most important part of the rocket. It’s something
a lot of teams get wrong. They’re so focused on making sure it won’t rip
As an avionics systems developer, I couldn’t agree more. Coleman flew home and I had to start preparing for the next two space-shot attempts with Operation Space.
Operation Space was a project started by
18-year-old Joshua Farahzad. It was collaboration of students from multiple
universities that had joined forces through the internet to design and build a
space-capable two-stage launch vehicle. They had reached out to me a few months
earlier about sponsoring their space-shot attempt and flying my avionics
package into space on their rocket. I saw it as an opportunity to get
additional testing and data on the Eagle system. Test it they did, in ways I
could have never imagined!
The first launch attempt was scheduled for Thursday morning at 6:00 AM. However, assembly of the first rocket wasn’t completed until late Thursday afternoon. Parts designed and manufactured in different parts of the country didn’t fit together the way they were expected to fit. Last minute modifications were required including additional machining of fins and other critical components. The avionics bay was completely redesigned on Wednesday and rebuilt on Thursday. The first deployment test didn’t occur until Thursday evening.
Friday morning, after 48 hours of
round-the-clock work, the first rocket was finally on the launch rail. Chase
once again sent the signal that ignited the first stage. Everything went well
until the sustainer engine ignited. It was obvious from the smoke trail that
the sustainer had gone completely unstable. Once it landed, we lost all
communication. Our search in the desert for the sustainer at the last received
GPS coordinates proved futile. At the time the leading theory was that the
sustainer had lost one of its fins.
The second rocket was launched Saturday morning. Its flight path also went unstable about two seconds after sustainer ignition. It also abruptly stopped transmitting all data once it landed. Once again, we went out to the last received GPS location. We never found the sustainer. However, to our surprise we did find the avionics bay with a short length of parachute tether and a wad of carbon fibers from the nose cone. When it hit the ground the battery tray inside broke loose and crushed my avionics system. Most of the SMT components had popped off the motherboard. Fortunately, the avionics bay was in a clearing only a few feet from where I had received the last packet during flight. Otherwise, we may have never found it since there was a lot of thick brush and we were all looking for a large rocket. We could have easily overlooked the small avionics bay hidden in a thicket. This is probably what had happened when we searched for the first sustainer the previous day. We had been warned not to poke around in the bushes because of the rattle snakes. We hadn’t considered looking for something as small as an avionics bay.
Once we returned to Mission Control, I was able to solder the SMT memory chip to a good Eagle motherboard using my hot air rework station. This made it possible to download the flight data. This is what the flight data revealed: two seconds after sustainer engine ignition, the rocket started to go unstable and then it drastically altered its angle of attack. One tenth of a second later, the avionics bay separated from the rest of the rocket. It did a 180-degree turn and coasted backwards to an altitude of 15.5 km (51,000 ft) with the parachute tether trailing behind it before coming back down. Most likely, aerodynamic loads at Mach 3.5 caused the carbon fiber nosecone to fail. This released the drogue which was housed inside the nosecone. The force of the drogue opening and shredding broke the altimeter bay free from the rest of the rocket. Later, I learned that the nosecones had a major manufacturing defect. There wasn’t enough time to manufacture new nosecones and those who knew about the issue had hoped for the best.
The Operation Space Team put in a lot of effort
to reach space. It was disappointing to see them only reach 15.5 km. However, I
have no doubt that with more experience, an improved design, and better
preparation, they can be successful. They had a lot of fun, worked well
together, and certainly learned many lessons. One in particular that I would like
You should never underestimate the amount of
time, effort, and diligence required for successful space flight. Among other
things it requires thorough engineering analysis, diligent acceptance testing
of all manufactured parts, exhaustive vehicle integration testing, and well-written
It was now Saturday afternoon. After downloading the flight data, I left Spaceport America with just enough time to drive back to El Paso and catch my flight. I only had one concern. With all the work helping Operation Space machine, wire, assemble, test, and prep their two rockets, I never did get my flat tire fixed. I was on my cellphone telling my wife how excited I was to see her and the kids that evening when a warning light went off. My adventures were not over: I had another flat tire!
About the author
Joseph Maydell has over a decade of both space flight and high-altitude ballooning experience. He is a former ISS Flight Controller and NASA spacecraft systems instructor. He has started multiple successful aerospace businesses and is passionate about inspiring students to pursue careers in space exploration. If you have any questions or comments, you can reach me here.