The RRS held it’s monthly meeting by teleconference on October 9th at our usual starting time of 7:30pm. We had a few members calling in from out-of-state. We had a few new topics to cover.
Some of the attendees to the October 2020 monthly meeting
SUMMARY OF RECENT MTA EVENT
We held a work event at the Mojave Test Area on October 3rd which was very successful despite higher temperatures for that autumn Saturday. We cleared a lot of tumbleweeds, mended the barbed wire fence at our front gate, painted the metal window gratings on the front of the Dosa Building and even cleared off the decks of the large vertical test stand. We had a lot of great help and we hope to continue making these site improvements to make our facility more attractive and useful.
The large vertical test stand at the RRS MTA after some clearing.
We agreed to meet at the MTA again on November 7th which will coincide with a static fire test of USC’s Rocket Propulsion Lab latest multi-grain solid motor design. We will also attempt to remove and replace a bent panel on the vertical thrust stand. The nitrous oxide hybrid rocket by Dave Nordling, Larry Hoffing and Osvaldo Tarditti is also ready for launching. If there are other member projects that are ready we will add those to the event and notify the pyro-op in charge.
LIQUID ROCKET PROJECTS
Liquid rocket projects have become more popular recently and some have started within the RRS.
Loyola-Marymount University (LMU) in Marina del Rey started a capstone project for their upper classmen in their undergraduate aerospace engineering program to design and build a large liquid rocket. The LMU Lion project was inspired by the FAR-MARS competition. Dave Nordling has been supporting the early design work on behalf of the RRS starting early this calendar year prior to the pandemic restrictions ending in-person meetings. LMU has restarted the project with the new academic year with a series of specialized coursework and short presentations on topics from experts around the industry. Dave was glad to present the history and capabilities of the RRS. The presentation was well received and LMU has looked at using our vertical test stand when they get their first liquid rockets systems ready for test.
Loyola Marymount Aerospace Research Society
The Compton Comet project at Tomorrow’s Aeronautical Museum has been restarted with RRS members, Waldo Stakes, Kent Schwitkis and Dave Nordling. The Compton Comet is a liquid rocket to be built, tested and flown at the RRS. It is a larger vehicle design which has several parts built and will use a surplus XLR11 single-chamber fueled by LOX and a 75% ethanol-water blend, It is a very ambitious project for the Compton College STEM students but it will provide an excellent means of learning practical skills.
Engine section built from a surplus tailcone and ethanol-LOX engine sits on the workbench
UCLA is continuing Project Ares for this next academic year. Last year’s liquid rocket vehicle design was in its final preparations for a Spring 2020 launch at FAR until the pandemic closed campuses around the country including the UCLA Lab. UCLA invited a few RRS members to attend their preliminary design review by teleconference. They are proceeding with several design improvements from last year’s vehicle design and when their laboratory access is restored under carefully regulated conditions, they hope to have another static fire at the RRS and flight from FAR next spring.
Thr Rocket Project at UCLA
Richard Garcia had started a design for a small liquid fueled rocket that would be easier to build and serve as the basis for a common or standard design for society members wanting to test and fly a liquid rocket at reasonable cost. Propellants are ethanol and liquid oxygen. The design has features proven from past successful liquid motor testing at the RRS MTA. The first prototype of the small 125 lbf motor is in build now. After successful demonstrations of the motor in hot-fire, the vehicle will be built.
Illustration of the RRS standard liquid rocket concept
There is a rocket hangar space opening up at the Compton/Woodley Airport which RRS members will soon have access. It has been a goal to have a work space within the city centrally located for most of our members. Operations at the rocket hangar will be limited to construction activities and small-scale pressure tests and cold flow operations, but it will offer our members a greater convenience for those with limited working space in their homes. Contact Wilbur Owens and Xavier Marshall for details. Social distancing and mask protocols would apply.
MTA FIREFIGHTING MEASURES
Fires are one of the greatest risks that come with amateur rocketry. At the behest of several members we have been discussing way of better preparing to fight fires from our site. The roughly one dozen pressurized water containers we have in our storage container are filled and made ready at every event. These have been useful for containing any fires starting at the pads. The RRS is looking at storing large quantities of water at the MTA. We’re also looking at trailer mounted water tanks that could be pulled by a small all-terrain vehicle (ATV) with a motorized pump spray system. These are commonly found in agricultural locations and would be an excellent addition to help limit the propagation of downrange fires until county resources can arrive.
An example of a 200-300 gallon water tank with a motorized pump system
MTA FACILITY UPGRADES
New restroom facility designs have been discussed over this summer. Concepts have been discussed with contractors and firm cost proposals are being prepared. Issues like cost and permits are important concerns. The society last year approved this facility upgrade project as the top priority.
One of several concepts for a new restroom facility at the RRS MTA under discussion
ANNUAL ELECTIONS FOR EXECUTIVE COUNCIL
Next meeting teleconference will be held on November 13th. After appointing an election chairman, we will be holding nominations for executive council positions at the meeting. Administrative members of society are encouraged to participate as we select our next year’s leadership. Active membership is also required so be certain to pay your dues if you haven’t all year.
If there are any questions or comments, please contact me RRS secretary. You can also follow the RRS on Facebook and on Instagram.
The long awaited work event at the Reaction Resesrch Society’s private testing site, the Mojave Test Area (MTA) took place as planned on Saturday, October 3rd. We had a good turn-out to take on a few of the much needed repairs, cleaning and maintenance activities around the site. These work events not only improve the site but also enhance it’s appearance for our visiting guests. The RRS takes pride in our one-of-a-kind site and working on our site makes us all more closely connected as public activities are so few during these unprecedented times. All activities were able to maintain social distancing and everyone had their mask.
The primary purpose of this event was maintence activities but secondarily we were ready to conduct launches if members had projects ready. I was the pyro-op in charge for that day if there was to be any launches. Wolfram had cancelled his first flight attempt of the Gas Guzzler two-stage rocket due to concerns with excessive heat. Also, my next attempt to fly my nitrous-oxide hybrid rocket was postponed as we needed more people to work the planned maintenance events throughout that day. Bill Inman had contacted me with his proposed solar heater experiment. After a cursory review of his experiment, the society allowed him to proceed. Bill makes a very long journey to the MTA from Carson City, Nevada, and we are glad he has chosen the MTA to conduct his initial experiments for his next generation steam rocket.
Osvaldo led the repair and refurbishment efforts that day. Despite the higher peak temperatures that day, a lot of work was done which has helpful in restoring the site.
The arched sign welcomes our membership and guests to the RRS MTA. Still looking great after years in the desert.
REPAIR OF THE 8-INCH ADJUSTABLE BOX RAIL LAUNCHER
The 8-inch adjustable box-rail launcher was damaged in a failed solid motor launch last year at the MTA. The resulting explosion destroyed the four adjustable rail guides and distorted a few of the box frame members. Given the heavy and large size of this box rail launcher, it was only practical to conduct repairs at the site and bring in new steel materials to be cut, grinded and fitted for welding such that all parts fit correctly.
Getting ready to build new rails in the 8-inch adjustable rail launcher
The replacement rail guides used thick square stock instead of the previously used round stock. This was done for both having a flatter surface for clamping and holding the rails in place but it also made moving the rails easier to do than with the closer fitting round rails. The square slider pieces were also more easily welded to the square rails with much grinding.
Osvaldo and Dmitri did excellent work. With the right tools, material and skill, the job was done by mid-afternoon. The four rails are back in place, but some of the box rail members remain bent or distorted. Although not entirely perfect, the rail launcher should now be useful again for future tests,
John Krell (left) and Dmitri Timohovich (right) inspect the repairs on the 8-inch box rail launcher at the RRS MTA on 10/3/2020
TUMBLEWEED AND BRUSH REMOVAL
A lot of the team was working on clearing the immediate area of tumbleweeds near the many structures and sites around the MTA. Alastair Martin and Keith Yoerg worked many hours with a metal rake and shovel and made a marked difference around several overgrown spots. Tumbleweeds are a persistent nuisance throughout the western United States and Mexico as they thrive in the dry hot climate. Removing them is fairly easy, but disposing of them is far more challenging. Fire hazards are one of the topmost concerns in amateur rocketry. Our desert launch site is always under this threat. By periodic clearing and disposal, the threat of fire propagation can be minimized.
Clearing the east side of the container fenced area.The large vertical test stand after some clearing efforts both on the ground and on the upper decks.Second view of the large vertical test stand at the RRS MTA at the end of our 10/3/2020 work event.Waldo drags an old iron launch platform to clear the vegetation from around the MTA site
Keith and Alastair did a lot of hard work in manually clearing the edges and the upper decks of the vertical test stand. Waldo Stakes was also kind enough to drag the area to clear wider spaces more quickly, The result is a clearer work area better able to conduct rocketry activities at the MTA.
CORROSION PREVENTION AND PAINTING
Frank Miuccio and Chris Lujan worked on the metal lattice covers on the two front windows of the Dosa Building. They sanded and brushed on rust remover to clear the surfaces for a protective paint coating, It was a lot of fine detailed work but the resulting look of the metal grates without rust looks so much better.
Frank carefully sands, treats and paints the metal lattice covering on the front windows of the George Dosa building at the 10/3/2020 MTA work event.Chris Lujan steps back from his work on the other front window of the George Dosa building.
Little touch-ups can be very time-consuming but it is worth taking the time to do the job well. There are many areas around the MTA that could benefit from some corrosion removal and surface protection. Although the desert is dry, the caustic, salty, dry lake environment can erode steel surfaces over the years.
SOLAR CONCENTRATOR EXPERIMENT
RRS corresponding member, Bill Inman came out to the RRS MTA work event to conduct a test of his first prototype solar concentrator for heating his next generation steam rocket. The experiment was a simple apparatus design to focus sunlight on a length of 2-inch black-painted iron pipe holding roughly 2,7 liters of water.
The wooden box had two angled mirrors to focus most of the incident sunlight near the pipe. To avoid natural convection losses, his concentrator had a clear glass panel enclosure. In essence it is a trough heater. The goal was simply to understand the practical operation of this first device and make improvements to see if a solar-based heating scheme for a steam rocket is feasible. Bill’s device had approximate pressure relief should the concentrator over-perform.
Bill Inman’s first prototype solar trough collector for heating a steam rocket tested on 10/3/2020
Results were a little lower than expected, but a measurable gain in water temperature was measured after operating throughout that afternoon, Air temperatures reached a peak of 104 degrees Fahrenheit (F) and the peak water temperature was 180F, far short of boiling temperature (212F) at amibent pressure. Effective steam rocket temperatures are often around 350F to 400F. There is more work to be done.
A FEW SMALL ROCKETS LAUNCHED
Keith Yoerg prepares the Big Bertha for launch on his wire rail launcher.
Keith Yoerg had brought a few small rocket kits for launching at the MTA during a break in the maintenance work. A classic Big Bertha and Baby Bertha each with B6-4 motors. The winds were very light and good for launching these small rockets. Both were ably recovered.
IDEAS FOR FUTURE WORK AT THE MTA
Near the end of the day, we discussed new improvement tasks at the MTA. A few of these were listed below:
Further removal and disposal of tumbleweeds, there are a lot along the eastern fence and in the flame bucket of the large vertical thrust stand. Burning them under controlled conditions is one possibility but winds must be very low
More ideas for the new restroom facility were discussed that could take advantage of pre-existing materials or assets at the MTA
Removal and replacement of the bent steel panel on the vertical thrust stand. New steel panels were made with the matching hole pattern.
Rust removal, corrosion prevention and painting of the large vertical test stand structure is a lengthy project but would greatly improve the look of the whole site.
Removal and replacement of the old blockhouse roof and shoring up the existing walls is being considered as a lower cost upgrade to this important and often used asset at the MTA.
Taking some measurements around the bent panel on the vertical test stand at the RRS MTA
It was a great team effort that day and everyone worked very hard. Nearly all of the planned objectives were accomplished. It has been suggested that another work event at the MTA be planned for next month. We also hope to work in a few launches if we can.
These ideas and other topics will be discussed at the next meeting of the RRS on Friday, October 9th. We’ll hold this meeting by teleconference again due to COVID-19 restrictions. Those wishing to attend should contact the RRS secretary.
In the absence of our secretary, I took a few notes from the meeting. This is what I recorded. Contact the RRS secretary for updates and corrections.
The Reaction Research Society held its monthly meeting by teleconference on August 14, 2020. Our monthly meetings are always held on the 2nd Friday of every month. We’ve had a lot of success with holding our meetings remotely and we will likely continue for the next coming months to continue our commitment to safety in light of the pandemic. Our membership is in regular contact with our community which has allowed us to promote and hold events including our first launch at the Mojave Test Area (MTA) on July 25, 2020. You can read the details in the firing report posted on this website.
Our members are doing well and thus far no one has reported being infected with COVID-19 which we hope continues to be the case. Frank is in regular contact with the Los Angeles Police Department’s (LAPD) Community Safety Partnership (CSP) but under current circumstances, the next school event may not be until next year. Options are being considered on how to continue our educational programs while maintaining social distancing.
The August 2020 RRS meeting held by teleconference.
REVIEW OF THE 7/25/2020 LAUNCH EVENT OPERATIONS
The first topic was the recent launch event we held on July 25th at the Mojave Test Area for the first time since the start of the pandemic. We had some difficulties in operating under the summer heat (106 Fahenheit at the peak) but this is nothing unusual for this time of year. Many of us were well prepared for the hot sun with our hats, sunscreen and iced beverages and chilled water. We also did a good job of watching out for each other. Still, the heat was responsible for leaving all but one of the micrograin rockets downrange. It also underscores the importance good planning, coordination and putting safety over all other considerations. We had several mis-fires which we were able to resolve, but maintaining discipline during the event proved to be a larger challenge. The launch protocols will be explained more thoroughly in the next safety briefing. The meeting highlighted that every member and pyro-op attending the event holds a joint responsibilty for the safety of all and it starts with self-discipline and patience by all.
Getting the beta rocket ready in the launcher on 7/25/2020 and setting the camera
We also discussed proper protocols such as announcing the pyro-op in charge well before the event and the necessity of providing detailed information about the intended operations to the pyro-op in charge in advance. Most of the planned projects were well understood as they were micrograin rockets and the previous hybrid rocket attempted at the last launch event.
DATA REVIEW OF THE STANDARD ALPHA FLIGHT OF 7/25/2020
The only micrograin rocket to be recovered from the launch event of 7/25/2020 was the standard alpha with plain steel nozzle. John Krell has been developing progressively better and more powerful avionics payloads designed to fit the narrow confines of the RRS standard alpha payload tube. John was able to spot and recover one of his payloads and process the flight data captured that day. The avionics payload was intact after being extracted from the desert floor including the solid-state data chip. John was able to recover the data and accurately reveal the huge acceleration of the RRS standard alpha with unprecedented accuracy. A peak acceleration of 114 G’s was recorded at roughly 0.3 seconds just before tail-off and burn-out at 0.4 seconds from launch. I was able to screen capture his plot below.
John Krell’s presentation of the data from the one recovered alpha ( to date).
The second plot shows the velocity derived from the accelerometer readings in the half-second which captures burnout at 0.4 seconds. Burnout velocity was measured at 670 feet/second which is consistent with prior data and trajectory predictions. The alpha is subsonic but travels at substantial speed from the swift acceleration. Given the high air temperature that day, 106 Fahrenheit, the speed of sound was 1165 ft/sec. The altitude of burnout was determined to be 130 feet which is consistent with prior flight data and high speed video footage.
Trajectory plot of the standard alpha flight from 7/25/2020
The third plot was made for the whole flight of standard alpha from the 7/25/2020 event from launch to impact at 35 seconds. Given the roets were impacting 2000 to 3000 feet downrange, the sound delay matches with the time to impact witnessed in the observation bunker. The maximum altitude was just over 4,400 feet based on the barometric pressure measurements using the 1976 standard atmosphere model. Base atmospheric pressure reading at the start of the flight shows the elevation of alpha launch rail platform is 2,048 feet.
Trajectory of the standard alpha flown on 7/25/2020
John Krell has really accomplished something with these custom avionics packages. He has been mentoring some of our other RRS members and the society encourages other members to build and fly their own payloads to spread the knowledge.
John Krell and Bill Behenna discuss avionics payloads
The society hopes to recover the other two alphas and the beta for further data analysis. Both of the unrecovered alphas from this last launch event had ceramic coated nozzles which should not erode. This should result in a more ideal performance as the throat area will not open up. The actual effect of this design improvement can best be assessed with recorded flight data. Also, we hope to compare the trajectory of the four-foot propellant tube with the standard length. Lastly. if the beta is recovered with recorded flight data, we may be able to assess its performance in unprecedented detail. The society hopes to report this flight data soon.
IMPROVEMENTS TO THE NITROUS OXIDE FILL/DRAIN MANIFOLD
The failure to launch the second build of the hybrid rocket was discussed at the August 2020 meeting. After discussing the launch procedures and corrective actions followed during the attempt to launch the nitrous oxide hybrid at the MTA with Osvaldo (the Level 1 pyro-op in charge) and racing experts at Nitrous Supply Inc., Huntington Beach, California, the cause of the fill valve’s failure to open became clear.
nitroussupply.com
In the racing industry, these normally-closed direct-acting solenoid valves are commonly used to open the flow of stored nitrous oxide bottles against the full supply pressure in the storage bottle. These are called “purge solenoid valves” among racers because it is this solenoid valve that opens the flow of nitrous oxide which displaces or purges out the air in the engine lines during the race. Buying these 12-volt DC high pressure solenoid valves from racing suppliers is much cheaper given they are made in greater numbers for the racing industry. (~$120 each versus $400+ each from reputable solenoid valve manufacturers).
In researching common designs for normally closed (NC) solenoid valves, the excessive heat of that day simply created too much inlet pressure against the internal valve seat for the electromagnetic solenoid coil to overcome and open the flow path. 1000 psig is likely the limit to reliably open these valves according to advice given by Nitrous Supply Inc. who has decades of practical experience at racing tracks around the country using purge solenoid valves for an application nearly identical to the needs of hybrid rocketry fill and drain operations. The ambient temperature at the MTA on launch day was creating a bottle temperature of 1400 psig accordling to the bottle pressure gauge and the separate pressure gauge in the manifold when the bottle was opened. This is well above the 900 psi recommended pressure range seen by marking on the gauge. The bottle, valve body and fittings are rated for these higher pressures, but opening mechanism of the solenoid valve was not.
A color-coded example of direct-acting normally closed solenoid valve is below. Blue shows the high pressure fluid path which is holding the seat down along with some assistance from an internal spring only for low inlet pressure conditions. With current applied to the electromagnetic solenoid (Orange), it pulls up on the moving armature (in red) which then allows the fluid to slip past the seal and through the flow control orifice when commanded open. Only a slight amount of movement is necessary to lift open the valve. However, if the fluid inlet pressure is too great, the solenoid can not provide enough force to lift and open the seal, therefore the valve stays shut.
Example of a direct-acting normally closed (NC) solenoid valve courtesy of M & M International (UK) Limited with color added to distinguish key parts.
To understand the relationship between pressure and temperature of the nitrous oxide you must consult the vapor pressure curve for nitrous oxide. This set of data points spans between the triple point and critical point of any pure fluid. NIST provides accurate data to generate such a curve.
webbook.nist.gov
nitrous oxide (N2O) liquid state properties, HTML5 table output from Web-book NIST.gov websiteNitrous oxide (N2O) vapor phase properties, HTML5 table output from Web-book NIST.gov website
The critical point of any pure fluid is where the distinction between gas and liquid phases disappears. This is not necessarily hazardous but it does mark a fundamental change in fluid behavior. The critical point of nitrous oxide (N2O) is 1053.3 psia and 97.6 degrees Fahrenheit according to Air Products company literature. This means the nitrous oxide conditions in the bottle at the launch (1400 psig as read on the gauges with an fluid temperature of 106 Fahrenheit or more) was well in the supercritical range, but again, this is only hazardous if the pressure vessels and plumbing connections aren’t able to safely contain the pressure. If the solenoid valve could have been opened, the pressure drop would have returned the supercritical fluid back to normal conitions and would flow dense liquid into the rocket when the fluid naturally chills down from the expansion.
Both the bottle pressure gauge and the manifold pressure gauge read excessively high on that hot summer day.
Keeping the bottle pressure below 1000 psia means controlling the external temperature of the bottle to a lower temperature. Below is a tabulation of state points along the vapor pressure curve for nitrous oxide (N2O) for common ambient temperatures. You can see that small shifts in ambient temperature can greatly affect the vapor pressure of the pressurized liquid. Keeping nitrous oxide under pressure is the key to retaining its denser liquid state. As long as the tank pressure is above the vapor pressure at that fluid temperature, you will have a liquid phase in the tank. If the pressure on the fluid drops below the vapor pressure, the liquid will begin to boil away.
30 F, 440.05 psia
40 F, 506.63 psia
50 F, 580.33 psia
60 F, 661.71 psia
70 F, 751.46 psia; liquid density 48.21 lbm/ft3, vapor density 0.1145 lbm/ft3
80 F, 850.46 psia
90 F, 960.09 psia
97.6 F, 1053.3 psia; density 28.22 lbm/ft3, CRITICAL POINT
Molecular weight = 44.01 lbm/lb-mol
Vapor curve for nitrous oxide over ambient temperature ranges
At first, it was thought that there wasn’t sufficient current from the lawnmower lead-acid battery we use. The summer heat can cause batteries to fail, but even after switching to a car battery, the failure to open was the same. Having a 12-volt solenoid requires greater current to actuate the solenoid valve, but it is a common standard for automotive grade parts which can be less expensive yet reliable. A current draw of 15 Amps over the long cable runs of a few hundred feet can be taxing to the firing circuit battery. This was not the cause of the problem, but it is a regular concern making sure sufficient voltage and current is available to both ignition and valve control.
To exclude outright failure of the solenoid valve, Osvaldo brought the unit home, allowed it to cool to room temperature then dry-cycled the valve from a battery to see if it still actuated. This simple test was successful and the filling valve in our nitrous oxide manifold continues to operate. At the next launch attempt, we will be prepared to chill the nitrous oxide supply bottle with an ice bath if necessary as was originally suggested at the prior launch event. Keeping the bottle pressure in an appropriate pressure range for fill operations is dependent on controlling the fluid temperature (60 to 90 F) under extreme heat or cold environments.
In researching purge solenoid valves, a second 12 VDC normally-closed valve was found and purchased. Nitrous Supply Inc., was out of purge solenoid valves but offered many alternative suppliers in the Los Angeles area. After some searching, I selected a high flow purge solenoid valve sold by Motorcycle Performance Specialties (MPS) Racing in Casselbury, Florida, for the purge solenoid valve used for venting our nitrous oxide manifold. The control panel is already equipped with the second command channel to open the vent from the blockhouse should it be necessary in launch operations. A schematic illustration is provided in this article.
mpsracing.com
Normally-closed 12 VDC purge solenoid valve from MPS Racing in Florida used for nitrous oxide applications including car and motorcycle racing.
The previous drain solenoid valve equipped with the nitrous manifold I bought was not deisgned for the full bottle pressure in the manifold so it quickly failed during initial checkouts. A manual valve was used in its place to carefully bleed out the remaining pressure in the line after the main bottle valve was tightly closed. This second solenoid valve will be used for draining the nitrous in the event of a launch scrub. Although the Contrails hybrid motor already has a small orifice and vent tube at the head end of the nitrous tank to provide slow release of pressure buildup, it is better to have a remote option to quickly depressurize the vehicle if the need arises.
Fill, drain and firing circuit for a Contrails hybrid rocket motor
With some re-plumbing of the nitrous oxide manifold to include the new vent solenoid, a soap-bubble leak check would be needed to prove the system before use. Given the significant overhanging weight of two solenoid valves, it may be wise to mount both valves on a separate plate structure to avoid excessive bending loads on the bottle connection. Design changes like this will be considered in preparation for the next launch event.
PYROTECHNIC OPERATOR TRAINING SESSION BY FRIENDS OF AMATEUR ROCKETRY
Mark Holthaus of the Friends of Amateur Rocketry (FAR) organization is offering an online training session for those interested in becoming licensed pyrotechnic operators in the state of California. The event requires registration on the FAR website and a fee paid to FAR ($10) to attend this two-hour introduction to the licensing and application process to be held on August 26th.
Friends of Amateur Rocketry website for indicating interest in pyro-op classes
Amateur rocketry in California is controlled by the same laws governing fireworks which require licensing by a state exam. The application forms and guidelines are available through the Office of the State Fire Marshal in the state of California (CALFIRE).
This training course for pyro-op applicants is another example of FAR and the RRS partnering to help the cause of amateur rocketry. The RRS, FAR and Rocketry Organization of California (ROC) last year met to create a joint set of recommendations to help CALFIRE improve the definitions used to govern amateur rocketry when CALFIRE they were seeking input from rocketry organizations. It is to the mutual benefit of the whole rocketry community and the public that there be more licensed pyro-op’s in amateur rocketry to both increase awareness of state laws and improve the culture of safety in our hobby and professions.
This FAR training course only serves to provide applicants with basic guidance on how to begin the application process and prepare to take the examination. Members of FAR, the RRS, ROC and any other amateur or model rocketry organization are welcome to apply. Several members of the RRS have already applied as the society continues its campaign to grow our ranks of licensed pyro-op’s at all three levels.
Completion of this training course does not substitute for any part of the pyro-op application process set by CALFIRE. As each applicant is required to pay their own fees including fingerprinting, they must also provide five letters of recommendation from licensed pyro-ops at or above the level of license being sought. After this class, each applicant must formally request these letters from state licensed pyro-ops in writing. For a licensed pyro-op to offer a letter of recommendation to an applicant, they must be willing to endorse their skills, knowledge and character to the state of California based on their personal experience with that individual. This is done through active participation at launch events through rocketry organizations having licensed pyro-ops leading their operations. Apprenticing, studying and attentiveness are all ways that a pyro-op can get to know an applicant personally and thus build confidence that the applicant is ready to have the responsibility of being licensed in rocketry. A letter of recommendation is given solely at the discretion of the licensed pyro-op which means their standards and expectations may vary significantly from others. It is important to establish a working relationship with both the society and the specific pyrotechnic operator over several projects to demonstrate skills and learn best practices through active participation.
As the RRS has more licensed pyro-ops than FAR at this time, this training course will be successful if both organizations support it. Some of the RRS pyro-ops have already offered their support as this means more people will need to become active with the RRS and conduct their projects at the MTA.
ROCKET LABORATORY AT THE COMPTON AIRPORT
Keith Yoerg announced that there is a tentative plan to create a rocket laboratory in a hangar at the Compton Airport, Although, the hangar will be used from time to time to store or service light aircraft, there is a great deal of working space which will help the RRS continue their liquid rocket project already underway. Several members of the RRS are also active with civil aviation and are members of Chapter 96 of the Experimental Aircraft Association (EAA 96). The EAA has generously supported the RRS over the last two years and we hope to continue and expand this partnership.
NEXT EVENT AT THE MOJAVE TEST AREA
The RRS has been planning the next event at the Mojave Test Area which will be dedicated to repairing some of our facilities including the adjustable rail launcher damaged in solid rocket launch explosion in August 2019. The consensus at the meeting was that we should not to return to the MTA for a formal launch event until the seasonal temperatures decrease from the excruciating desert summer. October 3rd was selected for this work event, Our hope is the weather will be cooler and we can accomplish more on that day. We may also take some time to search for more rockets planted downrange from past launch events.
The RRS may also conduct a few static firings or even a launch if member projects are ready. All such proposed hot-fire and launch activities must be proposed to the RRS president and the selected pyro-op in charge for that day. Some of our member projects such as Wolfram Blume’s Gas Guzzler two-stage ramjet and my second-build of the high-powered hybrid rocket are both still works in progress and may be ready for the early October launch date. Larry Hoffing has been working on an improved solid motor chemistry which he may want to test at the MTA.
The RRS is available for private events before that time, but one must make their request to the RRS president as usual. Some have indicated interest in returning to the site for just a few hours to recover more rockets downrange. Its our policy that at least two members be present for any excursions to the MTA and the RRS president must be notified in advance.
IN CLOSING
Some topics were not able to be covered including the overview of the new RRS Constitution as it gets ready for administrative membership review. Also, facility improvement plans at the RRS MTA including new restroom facilities and blockhouse should be discussed.
The next RRS meeting will be held by teleconference on September 11, 2020 as it is unlikely we will be permitted to return to the Ken Nakaoka Community Center by then. We hope everyone continues to stay safe during these days of the pandemic and try to stay in touch as we are planning another event at the MTA for October 3, 2020.
If there are any questions, please contact the RRS secretary.
