Solar Cat Steam Rocket Development: Part 1 (2020-2022)

by Bill inman, Reaction Research Society


During, and even before my first steam rocket, the “Scalded Cat”, first launched in 2000, I had contemplated the idea of heating the water with concentrated sunlight.  Also, in the years after the Scalded Cat, I became convinced that, as impressive as it was, it’s highest flight of 4660 feet still left room for improvement.  My late wife Carmela and I had discussed trying to combine an improved performance rocket and a solar heated rocket into one project and launching it on the 20 year anniversary of Scalded Cat’s first flight in December, 2000.  She was enthusiastic about the idea, but in 2019, died before it could happen, and I regretted her not living to see it.  As a new widower considering my options, I decided on this project for my next chapter in life.

Part 1 of the report on this continuing project covers the early development of a parabolic trough concentrating solar furnace to heat the water in a future steam rocket, and the results of the first “Solar Cat” rocket.


 Develop the knowledge and experience through hands-on design, fabricating and testing to eventually build and launch a 100% solar powered steam rocket with dramatically higher performance than the original propane heated “Scalded Cat” flown at the Reaction Research Society’s Mojave Test Area (MTA) in the years 2000, 2001 and 2002.

Some of my good friends have been a tremendous help along the way.  In addition to myself, “Team Steam” primarily includes (in alphabetical order):  Kime King-PatrawDave McKinnonKeith & Nadara SoulesDale Talcott, and Jon Wells

Launch of the Scalded Cat on it’s first flight, December 2, 2000.

Some of my friends and I have had an interest in solar energy since high school back in the 1970s, particularly in the heat potential of concentrating solar furnaces.  As such, we built several “science project” type models over the years – one reaching 600o F. – more than enough for a steam rocket.   Combining steam rockets with concentrated solar heat seemed like a good way to pursue both these interests simultaneously.

Receiver design with an upper window and two diagonal mirrors:

Before building the parabolic reflectors, I wanted to test an idea for the receiver since it will double as the launch pad and radiant heat collector. The receiver must be wide enough for the rocket fins to pass through for launch, it will cast a larger shadow than otherwise.  I hated losing that area of potential solar heat, and got the idea of trying to capture that otherwise lost sunlight from the top, with a window and  2 diagonally opposing mirrors inside, reflecting it onto the receiver tube.  The first device tested on October 3rd and 4th of 2020 was just a particle board box of this design.  (see cross sectional drawing below)

By itself, this receiver box was underwhelming, unable to even boil water in four hours of full sun.  Undoubtedly, there was significant heat loss on both ends of the receiver tube where metal fittings, valves & instruments protruded outside the box.  Wrapping those areas with makeshift insulation on the 2nd day’s test helped retain some of the otherwise lost heat, but it still fell short of expectations.

Testing the receiver box alone this way couldn’t tell us much though, since in this form, it was really just a small batch type solar water heater.  The real test would be comparing this design against one with the upper part just insulated instead,  and heated only by a parabolic reflector through the bottom window.

First of four pictures shows the 2” galvanized pipe receiver tube freshly painted with Thurmalox solar collector selective coating

Second photo of four shows the receiver box with the receiver tube and the two diagonal glass mirrors installed.

The third photo of four shows the reciever with an upper glass window, mounting yoke, instruments and a drain valve.  The receiver tube ends double as pivoting points for manually turning it to follow the sun

The fouth and final photo of the series shows the reciever assembly as it was set up at the RRS MTA on October 3, 2020 initially facing away from the sun before starting it’s first test.

The following graph shows the heating rate starting slower on the second day (blue line), but then picking up and passing the rate of the first day.  This was probably due to the start times.  The sun was lower in the east at the start on the second day and heating picked-up at mid-day.  

On the first day however, the sun was high at the start, but soon sinking into the west resulting in the heating rate dropping off after a period of two and a half hours.

The plot of temperature rise during the two tests on October 3rd and 4th of 2020.  The ambient air temperature was around 95 Fahrenheit.

Adding a four-foot span parabolic reflector focusing through the lower window:

This configuration was needed to actually test the difference in temperature achieved with and without using the top window and diagonal mirrors.  Not surprisingly, this version was able to produce higher temperatures than the receiver box alone, hitting the boiling point with ease.  However, when the use of the internal diagonal reflectors was compared with blocking the sunlight to them with fiberglass insulation, no discernible difference in heating was apparent.  And with larger parabolic reflectors planned, it seemed likely that the higher temperatures would result in larger radiant heat losses through the top window, exceeding any potential gain.  Therefore, this idea was abandoned.

​Adding the 4 feet of parabolic reflector involved enlarging the “U” shaped yoke to accommodate the corresponding increase in width and depth.  Trying to save the materials and work that went into the receiver box while continuing to use mostly surplus lumber for the project, still mostly particle board, yielded less than ideal results.

​However, we were now on to testing the outputs of the parabolic trough solar furnace, the actual objective.  The first test was attempted on November 7, 2020 at the RRS MTA, but clouds rolled in, blocking the sun until it was too low in the west to aim at.  So our first actual readings were taken with the 4 foot reflector back home in Carson City two days later.  

This version exceeded 300o F. twice, with a best of 371o F in 4 hours.  In both those tests, it reached 300o F within 2.5 hours with full sun.  In the other tests, clouds interfered, yet it still reached 267o F in one of them.  In all, 8 tests were conducted in this configuration, ending on November 23rd.

We also learned that heating was still possible in thin overcast conditions as long as the clouds were thin enough to allow the sun to create shadows with crisp edges.  But the heating rate was reduced, as was the stagnation temperature.

First of four photos shows the cutting out the parabolic curve in particle board.

The second of four photos shows the checking the focal spot on the ground with the reflector attached as seen by the intersection of the two bright lines.

Third photo of four shows the solar furnace set up but sitting idle at the RRS MTA on a cloudy day – November 7, 2020

Fourth of four photos shows another view of the assembly sitting idle at the RRS MTA.  Notice the absence of dark, crisp shadows due to clouds.

Same setup but with a larger reflector with two 3-foot spans:

​A primary goal of these steps of the project was to determine how hot the water in the receiver tube will get – and how fast it will get there vs. the size of the reflector, in both square footage and span (concentration ratio).  A number was derived from the tests with the receiver box alone, and now also from the 4 foot span reflector.  Of course, a foot wide swath right down the middle was shaded by the receiver box, so that area had to be subtracted from the total square footage.  By replacing the single 4 foot wide reflector with two reflectors, each 3 feet wide, a comparison was possible.  Also, the two reflectors were moved out from the center a few inches, reducing the amount shaded by the receiver box.

​Again, this particle board contraption was enlarged by adding about a foot to each end of the parabolic end boards to support the wider reflector.  Reinforcements were added to the yoke as well, because unlike the previous version which was hauled to the MTA disassembled in the back of my 2000 model year GMC Jimmy and re-assembled on site, the new 6 foot span and yoke would not quite fit.  Instead, it was rebuilt to sit on a platform on a utility trailer towed behind the Jimmy, but still transported disassembled.  Both the yoke and the reflector assemblies had also become so heavy and ungainly that it was getting difficult to assemble and disassemble without assistance.  Dimitri Timohovich offered to assist several times, and was a big help on those occasions.

New idea to add nozzle and fins to launch a demonstration rocket with the receiver:

Now, my late wife Carmela and I had had the idea to launch the new solar powered steam rocket on the 20th anniversary of the first successful Scalded Cat launch – the RRS December 2000 event.  It was looking like a lost cause until the best temperature and pressure achieved with the 4 foot reflector almost touched what we had considered the minimum needed for a steam rocket.  With the new, larger reflector, it should only do better.  By then, we were fast approaching the end of November, but what if?  … Could there be any possible way to do it that quickly?

Well, I had built and launched a couple of “Simple Cat” steam rockets starting in 2006, proving that a very simple rocket based on 2-inch nominal galvanized pipe with “hardware store” fittings and accessories, and released by a manual “pull cable” could actually fly.    One even reached approximately 1000 feet of altitude according to MaryAnne Butterfield’s calculations from it’s flight time.   And the receiver tube in this solar furnace experiment was already none other than 2” galvanized pipe!  Could the receiver box be made into a launch pad, and the receiver tube made into an actual flight vehicle?  – a solar heated “Simple Cat”?  That might just be the one chance we have to do this in under a month, making a December, 2020 launch possible!

​The first of two photos by David Allday shows the author by the “Simple Cat” in the tower on December 2, 2006, at the RRS MTA.

The second of two photos by David Allday shows the launch of the Simple Cat from the Large Vertical Test Stand at the RRS MTA on December 2, 2006.

The team’s decision was, “go for it!”  There was already a launch set for December 12th at the MTA, so that would be the target date – the official RRS December launch 20 years after our first steam rocket flight!  The fins and nozzle off the old Simple Cat were installed, and thanks to Dale Talcott’screativeness and fabrication skills, fin slots cut into the upper (north) end of the receiver box, and a launch tower added during a marathon session the weekend before the launch!  Provisions were also made to tilt the assembly far enough “south” to raise the tower & rocket vertical for launch.  Racing the clock, a lot was hurriedly done and not fully tested in the final form, if at all!   At the MTA on the 12th, we discovered that the newly reinforced reflector assembly was then too wide to fit into the newly reinforced yoke!  – OOPS!!!   With the quick thinking of Dave McKinnon and Dave Nordling, the yoke was hastily widened thanks to Dave McKinnon’s skills and cordless tools he had brought with him to the MTA.  But by the time we got it ready to start heating, the sun had moved behind clouds in the western sky.  – No 20th anniversary launch.

Or might there be…?   Back home in Carson City, Nevada, Kime King-Patraw pointed out that we still had nearly 3 more weeks left in December, and that launching it at ANY time in December of 2020 was still pretty close to the 20 year mark!  It wouldn’t be at an official RRS event at the MTA, but you can’t always get everything you want!  Some additional work was done, and heating tests were conducted on the 18th, 19th, and 20th, with the highest temperature reached being only 300o F.  All three were done in my backyard though, where shading from the bare trees and/or clouds still hampered the effort.

On December 21st, full of optimism, Kime and I drove to Tonopah, NV near where an undisclosed launch site had been chosen.  This area seemed fitting, as the 110-megawatt Crescent Dunes concentrating solar-thermal molten salt powerplant was also in the “rough vicinity of Tonopah”.   Jon Wells drove up from Las Vegas to complete our trio.  

The morning of December 22nd dawned completely cloudless in the high desert sky.  We drove out to the launch site early and set up.  Heating went quickly, but as pressure built, a drip started in the nozzle plug assembly.  We aborted heating, inspected, then cleaned & re-tightened the fittings involved, then re-filled and started the heating again.  Again, it started to drip once it started building pressure.

​By then, we didn’t have time to go back to town & look for a new fitting, but since the temperature and pressure continued to climb, even with the leak, we decided to just keep heating and see what happened.  As usual, the drip got worse as the pressure increased, and as it approached launch pressure, we started fearing it was almost out of water, too.  – So, knowing we’d need to release pressure and drain it anyway, and with nothing really to lose, we attempted a launch.  After a few tries, the stubborn plug/clamp finally released and it took off, becoming what just might be the world’s first ground launched, completely solar powered rocket!  – Nevermind that it was only at 175 psi and only went about 20 feet high on it’s half a pint of remaining water – it still cleared the tower!  – Hey, Dr. Robert Goddard’s first liquid rocket flight only went 41 feet high!

First of three photos shows the trailer mounted solar receiver at the RRS MTA on December 12, 2020. The only problem was no sunlight.

Second of three photos shows Kime King-Patraw and Jon Wells comparing notes during the heating experiment on December 22, 2020 conducted in the general area of Tonopah, Nevada.

Third of three photos shows the author conducting the first launch of a completely solar-powered, ground launched steam rocket just as it clears the launch rails.

Developing a motorized tracking system:

By manually adjusting the solar furnace to keep it targeted on the sun, it was necessary to move it and re-clamp it every 3 to 4 minutes.  This required someone physically being there to make repeated adjustments at that frequency.  The RRS pyrotechnic operators in charge took a dim view of this, and strongly advised us to come up with a remotely operated sun tracking method.  We had also been foiled in our tracking efforts at least a couple of times by other peoples’ projects needing us to take cover in the bunkers during their fueling, firing and/or troubleshooting.  This sometimes caused sun tracking to stop for an hour or more.

​I had once built a drive gear for a telescope mount with a clock-rated a/c gearmotor, so built one for this solar furnace using the same motor and concept.   Of course, this resulted in more pieces scabbed onto the monstrosity that was never originally designed for it, adding complexity, weight, and more potential problems.  In the end, this tracking gear worked … sort of…  We intentionally designed it to run “fast”, thinking it would be better for it to “outrun the sun”, allowing us to just momentarily stop it (with an “on-off” switch in the blockhouse) long enough for the sun to catch up, than risk it “running slow”, requiring approaching it to re-set it ahead by hand.  Again, that worked too … sort of…  It ran so fast that it had to be stopped for the sun to “catch up” about every 20 minutes.

​There were several other problems with it binding, hanging-up, and engaging/disengaging the gear teeth.  The rough road to the MTA broke the actual motor mounts one time, requiring a hasty field repair by Jon Wells and Dave McKinnon.  It had also become painfully obvious that the mount’s range of east-west motion was another limiting factor.  We never got set up too early to aim at the morning sun in the east, but there were several times we reached our western limit before the heat and pressure were sufficient, and the sun was still high enough that we could have kept going if only it was able to rotate farther west.  This wasn’t a fault in the tracking gear, but in the design of the mount itself.

​Along with a couple more unsuccessful launch attempts, mostly due to clouds, we still managed to make three more flights while also recording additional heating data.   It’s second flight was on March 20th at the MTA, again only reaching about 25 feet after more problems, including the broken tracking motor mount.  Dave McKinnon and Jon Wells both came again to assist on that attempt, Dave recording the heating rate notes, this time.  The 3rd flight was also it’s best, reaching an estimated 400 feet on April 1stat another undisclosed site, this time in “the rough vicinity of Lovelock, NV” where Dale Talcott and his brother Dave were able to attend.  Everything went right that time, other than a breeze and some high, thin clouds building, eventually slowing the heating rate.  My estimated potential of this fat slug of a rocket was it reaching 500 feet of altitude based on it being half the capacity of the earlier 6 foot long “Simple Cat-2” that may have reached 1000 feet of altitude.   An altitude of 400 feet wasn’t too far short of that estimate!!

Then it was back to the MTA for the fourth and what would be the final flight to another disappointing altitude of only 65 feet (again, derived  from timing it’s recorded flight duration).  – Clouds again…  Along with the ever faithful Jon Wells, Keith and Nadara Soules were present for this flight and kept a constant supply of energy bars and cold water bottles on hand.  They also helped clean the reflector, fill the rocket, and take care of trash.

First of four photos shows the Solar Cat reaching a height of 25-feet at the RRS MTA on March 25, 2021.

Second of four photos shows RRS member, Jon Wells, fielding questions at the RRS MTA. Note the new paint job on the receiver and tracking drive system.

Third of four photos shows the launch with the highest altitude on record of 400 feet on April 1, 2021 from just outside of Lovelock, Nevada. RRS member Dale Talcott can be seen to the left taking video of the launch.

The fourth of four photos shows the highest flight of the Solar Cat from the RRS MTA on April 10, 2021, reaching a height of 65 feet.

The device was being stored on my trailer in my back yard, oftentimes uncovered.  As the winter progressed, we had some rain and snow.  For protection – as well as aesthetics – we decided to paint it.  But what color?  Since the ultimate “improved performance rocket” would also be a tribute to my late wife Carmela, I asked her good friends Kime and Nadara what they thought Carmela’s favorite color was.  The answer was a certain shade of green. I had not known that, but they were both sure of it.  So Kime met me at Home Depot, and we picked out a color that was an ever so slightly lighter shade of what they both swore was Carmela’s favorite.  That’s how the color choice came about.

Developing data on heating rates versus reflector area:

Although we got a bit caught-up in trying to launch, certainly good experience to have before progressing to the ultimate “higher performance rocket”, the original purpose of collecting test data was never forgotten.  And while we collected heating data during these launches, most of it came from non flight heatings done strictly for the data.  We got in a total of 13 tests with the 6-foot span version between December 18, 2020 and April 18, 2021.

​We wanted to get the average of at least three “good” heating sessions for each of the three configurations to increase the confidence level of the averaged results.  With the constant problems being presented by tree branches, clouds coming out or the sun getting too low in the west to continue tracking, some of the results were settled on with less than 3 tests (marked by the dotted lines on the following graph).  Only two tests were conducted with the receiver box alone, because after the dismal performance, continuing seemed pointless.

​Also, while I’ve been referring to the 12-inch wide receiver box, the first 4 foot reflector, and then finally the two 3-foot reflectors (making a 6-foot total span), it’s important to account for that not being the actual “perpendicular intercept” of the sun’s rays.  For that, we need to subtract the width of the receiver box’s shadow, and the amount the reflectors are effectively shortened by their curvature.  The actual intercepted span of the receiver box is therefore, 8 inches, the “4 ft. mirror” is 34 inches, and the “6 ft. mirror” is 50 inches.  See the prior cross sectional drawing for illustration.

​And while we managed to get the “rocket” – actually a very heavy piece of 2 inch galvanized pipe with end fittings – off the pad and into the air 4 times, it’s clear that even with the 6 feet (actually 50 inches) of total reflector span, it was still pretty under-powered, requiring really good conditions to achieve launch.  The new “2nd generation” rocket and solar furnace with ten feet of total reflector span, should be a different story!

The results of the entire heating experiments over different spans of heater with projected curves.

Testing the commercial “Sun-Tura” 2-axis sun tracking system:

At some point, a novel idea occurred: “with all the solar activity going on these days, what if a commercial tracking system existed that we could just buy?”  A few Google searches eventually revealed the SunTura unit, and one was ordered.  

More headaches accompanied mounting it to the existing solar furnace, but it was eventually installed and operational … sort of …  The sun sensor when mounted as instructed, pointed the unit far to the east of the sun – about 25 DEGREES east of it!!!  The instructions said it could be adjusted by bending the stalks holding the little LED’s under the dome.  That idea made us pretty nervous though, as it seemed that getting it “right” on the first couple tries was unlikely, and too much bending could easily result in breaking something!

So several cardboard wedges to just sit the sun sensor on were made and tried until we found the angles that caused it to aim much better.  From this, the plan became making a more permanent version of this “mounting wedge” adding fine adjustment screws, in a manner borrowed from survey instruments Jon and I used a lot in the past.  Thus the last duty of the 1st generation solar furnace became to test the new sun sensor mount for the 2nd generation solar furnace.

This new mounting platform with adjusting screws was finally made, temporarily installed and tested, in August of 2022.  As hoped, it showed that it could be “dialed-in” to finally allow the SunTura sun tracking system to keep the assembly aimed at the sun accurately enough for our purposes.

The extreme angle of the cardboard wedge needed to correct the sun sensor’s output to have proper aim.

The new adjustable sun tracker mounting.

Now, with it’s last “assignment” finally completed, the battle weary Gen-1 solar furnace was mostly dismantled and removed from the trailer, clearing the way for construction of the new “Gen-2“ to begin.  Many of the screws and boards, many of them already “recycled” for this structure, were saved to possibly be used yet again in the future.

Jon Wells had come and stayed with me a few days, and was a huge help in this effort, including helping guide the decision that we’d leave a couple parts more-or-less intact to preserve some tangible evidence of this device: the two ends of the mount/yoke & the splice Dave McKinnon put in to adjust for a mistake of mine, and the launch tower that Dale had integrated into the receiver box so well that something would need to be cut to ever remove it.  Jon and I decided NOT to cut and remove it, but leave those last couple parts attached as testament to Dave’s and Dale’s creative solutions to make a solar powered launch on the 20 year anniversary of the original Scalded Cat’s first flight a reality.

Photo taken of the remaining pieces from the 1st generation Solar Cat receiver now sitting in storage.

This is a work in progress. Further updates will be reported as the Solar Cat project continues.

October 2022 meeting

by Dave Nordling, President, RRS.ORG

The society met at the Compton Airport front office again for our monthly meeting on October 14th. Mike LaGrange joined us by teleconference for the first time. Joel Cool-Panama was welcomed as our newest administrative member.

We first reviewed past events,

  • USC RPL sample grain burns
  • pad anchor modifications
  • restroom progress at the 10/1/22 work event

We spoke of pending events

  • Bill Claybaugh’s new pad, 10/20-10/22
  • Aerospace Corp launch of experimental motor, 10/20
  • next work event, 11/5-11/6, more plumbing
  • USC RPL static fire on 11/12
  • Events subject to change, public calendar soon to come online with the new website

The RRS reported quarterly dividend from

Further concrete repair work is needed. Four of the 28 mounting holes need more work. This will likely be done by the society. We need to determine best way to extract old anchors and patch the holes with sufficient time for curing before redrilling. USC RPL will assist by drilling final anchors once repair work is done. USC has been very helpful in making this important site improvement.

A budget update on restroom with expenses to date and how much to finish. Last estimate showed we’re on target. An update is coming before next month. Our goal is for the restroom to become operational by year’s end.

The society is working hard to help other members to become pyro-ops. More pyro-ops means safer operations and greater flexibility in future events. Frank and Bill Inman have their letters and are working on their applications. The best way to start is being active with society events and apprenticing under experienced and licensed individuals.

RRS has updated their flight waiver with the FAA to 100,000 feet. Some planning and advance notice required. Laminated copy of our waiver and instructions will be put in the Dosa Bldg. Also, launch requirements available from the RRS president.

Patrick Finley of the Collegiate Propulsive Lander Challenge attended. He explained his foundation to encourage propulsive landing technologies among university groups. Five technology prizes. The RRS is a supporter of this initiative. He can be reached at “”

Wolfram Blume has been working on the Gas Guzzler over the summer. Fuel pump and flameholder fixes. Next flight could be in December?

Bill Inman is building the 2nd generation Solar Cat with fellow member Dale Talcott in Nevada. Subscale prototype built in the summer had excellent focus and heating. Next test at MTA could be December, perhaps January.

John Krell’s avionics chips have had some improvements. Now can do 16 channels at over 1 kHz all on a chip fitting in a slim alpha payload tube

First meeting with LACMA by the president and VP on a STEAM project focused on the arts. Further discussions will better define the RRS role. 

2023 Symposium will celebrate our 80th anniversary, tentative date is April 8. Researching locations, food service and potential speakers. Official launch will be in the new year.

New launch rail design proposed for high power rockets using 24-feet of 1515 launch rail and a 1-ton hand-winch to operate. It will be an outdoor fixed asset and supplement existing launch rails. Need to get a materials list and drawings made for a contractor quote.

Larger 60-foot launch rail for liquid rockets is in the planning stages. The RRS has had several entities interested in using such an asset.

We will soon be starting the effort to sort out the old equipment in the north yard, determine the purpose, origin, and dispose or refurbish each item. We must use our space wisely and not store articles without a relevant purpose. Junk will always fill a void.

RRS may be getting a new pair of storage containers and fire-fighting equipment. Council is in discussions and supportive of this site improvement. More details later.

Some at the meeting indicated strong interest in learning how to weld. The RRS is seeking an instructor which may give us training for a nominal fee. More on this next month.

3D printers were discussed near the end of the meeting. Several members have the devices, but design tools are just as important. Google Sketchup, Solidworks and CATIA are options but costs on some can be prohibitive. This would make a fine topic for a future article on RRS.ORG

Nominations for executive council offices will be at the November meeting next month. An election chairman will be appointed who is neither a current office holder or a candidate for office.

Next meeting at Compton Airport front office on 11/11/2022 at 7:30pm.

MTA launch event, 2021-05-01

by Dave Nordling, Reaction Research Society

The Reaction Research Society held an event at the Mojave Test Area (MTA) on May 1, 2021. Dave Crisalli was the pyrotechnic operator in charge. RRS president, Osvaldo Tarditti, was also present along with myself, It was not to be a launch event as all planned tests were static firings by the UCLA liquid rocket team and the UCLA hybrid motor team. The winds were very high that day consistently above 20 MPH and gusts above 50 MPH at times. The weather otherwise was very cooperative with comfortable temperatures.

Other than gusting and persistently hugh winds, it was a great day at the MTA on 5/1/2021

Dave Crisalli gave a safety briefing in the George Dosa building to all attendees before the first static fire campaign would begin. The RRS pyrotechnic operator in charge is responsible for the safety of all during the event. Hazard identification (spiders, snakes, sharp objects) and good practices (hydration, sunscreen) are always part of the briefing, One of the most important things, Dave Crisalli mentioned was not to be in a hurry. It is very important to take the proper time to do things correctly and safely even if it means not proceeding with the intended test that day. Taking your time means avoiding mistakes and improving your chances for success.

Xavier Marshall observes the UCLA hybrid motor controls setup at the RRS MTA on 5/1/2021.

RRS members, Bill Inman and John Wells came to the MTA for the event, but only as spectators. The Solar Cat project is still active and undergoing improvements to its sun tracking method. Bill is also expanding the collector area and adjusting the necessary support structures. It is likely Bill and John will be back for the next RRS MTA event.

Dave Crisalli (left) and Bill Inman (right) at the RRS MTA vertical test stand on 5/1/2021

Also in attendance was the Compton Comet team who have all recently joined the society as members. It was their first time visiting the MTA and getting a chance to see another university team conduct liquid rocket test operations at our vertical test stand.

Members of the Compton Comet team, Manuel Marquez, Aarington Mitchell, Tre Willingham (from left to right) wait at the Observation Bunker at the MTA for the hybrid motor firing with Waldo Stakes (at right).

RRS member, Wolfram Blume came by the RRS MTA to take measurements of the vertical test stand for a future static fire test of his ramjet upper stage engine. He intends to use a leaf-blower compressor motor to simulate foward air flow, but a lot of calculations and planning is required before proceeding. The vertical test stand has a winch and pulley system still attached from Richard Garcia’s liquid motor test in 2017. It should be adequate for Wolfram’s lifting needs when mounting the test equipment to the stand.

The vertical test stand with the winch and pulley system still mounted.

The UCLA team spent the night before on our site setting up their equipment. This advanced planning paid off as they were ready for the first of two hot-fires of the liquid rocket just past noon.

Camera adjustments made before the first hot fire of the UCLA liquid rocket on 5/1/2021

Often, it can take several hours to verify all systems are in good working order before testing especially with a liquid rocket, The hybrid rocket was no exception that day.

The UCLA hybrid motor team installs the fuel grain and nozzle into the 98mm standard motor casing,
The UCLA hybrid motor mounted for static fire on the RRS MTA I-beam

One of the two load cells had failed so the two teams had to share the same load cell between the hybrid motor and liquid motor firings. UCLA chose to let the hybrid team go next after successful results were seen with the first firing, The UCLA hybrid motor team corrected a few issues and were able conduct a successful hot-fire by late afternoon.

The society members in attendance also had time to make some minor repairs to the new mobile trailer asset, A steel plate was added to keep intruders from entering. Thanks to Waldo Stakes for doing the welding for this temporary fix.

The mobile trailer at the RRS MTA needs a lot of repairs

There was sufficient daylight remaining for a second hot-fire of the UCLA liquid rocket, The team had another engine with the previous injector design from last built and ready with a fresh internal ablative liner. They had retanked another load of ethanol and the liquid oxygen cylinder had sufficient stores for another loading cycle.

Preparing for liquid oxygen transfer to the propellant tank

Thanks to the hard-won, acquired experience of the UCLA team and their commitment to training new members and holding to their proven procedures, they were able to conduct the second firing safely for an impressive finish that day.

The UCLA liquid rocket team poses before their liquid rocket after a second successful hot fire on the same day.

Initial data from both UCLA static firings of their liquid motor suggest that the 650 lbf nominal thrust motor outperformed expectations and will be ready for vehicle integration and flight by May 29, 2021. The UCLA team had reason to celebrate at the end of the day. The RRS was glad to be a part of UCLA’s continued campaign to fly liquid rockets that are competitive with any university team in the country.

For other universities interested in working with the RRS, please contact the society president submitting a Standard Record Form downloaded from our website,