Mike Paluszek of Princeton Systems, Sam Cohen of the Princeton Plasma Physics Laboratory and Charles Swanson also of PPPL attended the US – Japan Compact Toroid 2016 meeting in Irvine California this past August.
We presented papers related to Sam’s Princeton Field Reversed Configuration nuclear fusion reactor research program. Charles presented, “Extracting electron energy distributions from PFRC X-ray spectra,” Sam presented “Long pulse operation of the PFRC-2 device” and Mike presented, “Fusion-enabled Pluto orbiter and lander”.
Here are the workshop attendees.
It was fascinating to listen to all of the papers at the workshop! John Santarius, who has done cutting edge work on space propulsion and small fusion reactors presented his talk, “Aspects of Advanced Fuel FRC Fusion Reactors.” He gave a very informative overview of small fusion reactors and advanced fusion fuel technology. Thomas McGuire discussed the Lockheed Martin research on small reactors. There were several presentations by Tri-Alpha Energy scientists on their beam heated FRC.
We look forward to the next Compact Toroid Workshop!
My name is Matthew Daigger and I’m a mechanical and aerospace engineering major at Princeton University going into my senior year. I was given the opportunity to intern and learn at Princeton Satellite Systems this summer. Through this internship, I got a lot of valuable experience in 3-D modelling, research and design. I was able to work with the fantastic engineers at Princeton Satellite Systems as well as Princeton Plasma Physics Lab, who helped whenever questions in their areas of expertise arose.
DFD CAD model generation by Matt Daigger
The Direct Fusion Drive (DFD) is an innovative and exciting new technology being designed by Princeton Satellite Systems. This Rocket engine utilizes the Princeton Reverse Field Cycle fusion reactor setup in order to create both thrust and power for a satellite. The vehicle it is currently being designed for is an exploratory satellite being sent to Pluto. What makes the DFD unique is that it can potentially halve the flight time to Pluto, from ten years to five, as well as have enough fuel left to put the satellite into orbit. Along with this, the craft should have enough extra power to deploy a rover to the surface of Pluto and power a drill. This technology could also open other exciting doors, such as manned missions to Mars, given its capability to cut travel times so drastically.
The first task I worked on this summer was looking into how to incorporate a Brayton cooling cycle into the design of the DFD. This Brayton cycle had a dual purpose. The first is to help cool the reactor and prevent too much heat and radiation from escaping and potentially damaging other parts of the satellite. The second function is to re-use this waste heat and convert it back into usable energy. Two simple brayton cycles running in parallel were chosen in order to maximize heat absorption from the reactor and power developed. The working fluid, its flow rate and the diameter of piping, as well as approximate dimensions of the turbine and compressor were also determined. Another important design factor is the ability for the satellite to withstand launch loads. Preliminary launch load calculations were also done in order to get a better idea for the stresses involved with launch using a Delta IV Heavy launch vehicle.
All of this information helped to conceptualize the physical design, which was drawn up in Inventor. The shielding and incorporation of the Brayton cycle flowing through the shielding were ideas which were confirmed by members at PSS and PPPL. The length of the reactor is a key factor in determining how high energy it will be. The length was chosen so to produce a 1 MW engine. The superconducting coils were also a main topic of research. These are active superconductors which are used to shape the plasma. This is still an ongoing process, as using active coils hasn’t been done before, and our engine has unique weight and size limitations which other similar lab reactors don’t. The debate as to whether to use high temperature or low temperature superconducting coils comes down to total size and weight, including that of a cryo-cooling system in the case of the low temperature coils. High temperature superconducting coils are the more massive option, which generally makes them less desirable for space application. The support structure was designed to keep the size compact while being able to handle the stresses calculated earlier. All information about the RMF heating coils, which are used to actually excite and drive the plasma, was received and confirmed by colleagues at Princeton Plasma Physics Lab. The separation coils at the tail-end of the thruster are power variable, and allow the expelled products to be manipulated, giving the engine high precision control in space travel.
Overall, this was an incredibly interesting and educational experience. The work that the Engineers are doing at PSS is innovative and exciting. The big ideas that are being developed here today are what lead to the next big step in space travel tomorrow. I am very thankful for the opportunity to spend my summer here and learn from some of the best engineers in the industry.
On Tuesday, August 23rd I had the privilege of giving my talk on our Fusion-Enabled Pluto Orbiter and Lander at the 2016 NIAC Symposium. The video of the LiveStream is now archived and available for viewing. My talk starts at 17:30 minutes in, after Michael VanWoerkom’s NIMPH talk.
The talk was well-received and we had some good questions from the audience and the LiveStream. In retrospect I did wish I had added a slide on our overall program plan in terms of the PFRC machine and temperature and field strength, since I got quite a few questions on those specifics at the poster session. PFRC-1 demonstrated heating electrons to 0.3 keV in 3 ms pulses. The goal of the current machine – PFRC 2 – is heating ions to 1 keV with a 1.2 kG field. The next machine I refer to in the talk, PFRC 3, would initially heat ions to 5 keV with a 10 kG field, and towards the end of its life we would push the field to 80 kG, heat ions to 50 keV, and add some helium-3 to get actual fusion events. The final goal would be 100 second-duration plasmas with a fusion gain between 0.1 and 2. A completed reactor would operate in steady-state.
Thank you NIAC for this opportunity!!
I had a great time at the NIAC orientation in Washington DC last week, where I got “mugged” with program manager Jason Derleth:
Stephanie receiving her NIAC mug from Jason
The meeting was at the Museum of the American Indian, which was a great venue with so much beautiful art to see, and a cafe featuring unusual native foods from across America (elderberry sauce on the salmon). I had the opportunity to meet the other NIAC Fellows, and put names and faces to the other creative projects selected, as well as meet the illustrious NIAC external council. These experienced folks provide advice and encouragement throughout the NIAC process from their experience as physicists, engineers, biologists, science hackers, and even science fiction authors.
I have to say, my poster on the fusion rocket engine was popular, and everyone wanted to know how it works, why it hasn’t been funded already, and how soon the engine can be ready. Of course, we have yet to actually demonstrate fusion using Dr. Cohen’s heating method, but that is why we need the NIAC study – to flesh out the science and engineering of the rocket application to help bring in funding for building the next generation machine. And yes, let’s get to Pluto in only 4 years the next time! I’m really looking forward to working on the project in the next few months and presenting it at the NIAC symposium in August!
We just discovered that our NASA NIAC project on the DFD mission to Pluto was covered in a SciShow episode from June 14, 2016.
Hank Green does a great job talking about our project, and I love that he called it a “Pluto Explorer”, which rolls of the tongue better than “Pluto Orbiter and Lander”. However, he did get our fuel wrong: we are using deuterium and Helium-3, a reaction which produces no damaging neutrons. Hank cited “two types of heavy hydrogen”, which would imply deuterium-tritium fusion; this produces most of its every in very damaging neutrons, and is a reaction we go to great lengths to avoid in our machine. There will always be some tritium produced from the side reactions of deuterium with itself, but our machine is designed to exhaust it before it can fuse.
The comments from the viewers were interesting, including several along the lines of, “wait, did I miss fusion becoming a working technology?” Of course the fusion rocket is still theoretical, but it’s based on a real plasma heating experiment going on now at Princeton Plasma Physics Lab! And its true that many people don’t realize that fusion itself has been achieved in many machines, just not break-even fusion. Our machine is very different from the large tokamaks most people are familiar with.
We are very pleased to announce that Ms. Stephanie Thomas of Princeton Satellite Systems has been selected to be a 2016 NIAC Fellow. This Phase I study, entitled “Fusion-Enabled Pluto Orbiter and Lander,” will explore the possibility of using Direct Fusion Drive (DFD) to deliver an orbiter to Pluto complete with a lander. DFD is a fusion propulsion concept built upon a small, clean field-reversed configuration fusion reactor with a naturally linear geometry. The reactor becomes a rocket engine when additional propellant flows through, providing power as well as propulsion in one integrated device. This engine could halve the transit time to Pluto to 5 years from the nearly 10 years needed for New Horizons, while delivering 1000 kg worth of payload into orbit and providing up to 2 MW of power. This will enable remarkable data collection such as high-definition video and drilling into the planet’s surface. The technology provides a path to terrestrial fusion as well as eventual human missions across the entire solar system. The Phase I study will focus on creating higher fidelity models of the engine performance to enable optmization of possible mission trajectories and better quantification of the predicted specific power.
The Galileo moons of the Jovian system are of great interest for future space exploration due to the belief that three of the four of the largest moons (Europa, Ganymede, and Callisto) contain water (in liquid and/or ice form). So far the eight spacecraft that have visited the vicinity of Jupiter are Pioneer 10 and 11, Voyager 1 and 2, Ulysses, Galileo, Cassini, and most recently New Horizons. NASA has ambitions to send another probe to further study Europa.
At Princeton Satellite Systems, in collaboration with Dr. Samuel Cohen at the Princeton Plasma Physics Laboratory, we’ve been working on the Direct Fusion Drive (DFD) engine, an advanced technology for space propulsion and power generation. Using the DFD, we have simulated two potential missions to Europa, an orbiter mission and a lander mission. The simulations were completed in MATLAB using functions contained within our Spacecraft Control Toolbox.
Sam Cohen and I were interviewed by Princeton University’s radio station, WPRB 103.3 FM. You can hear the broadcast here:
WPRB 103.3 FM DFD Broadcast
The show is 3 hours long because it includes musical selections.
Explosions. Orbits. Stuff hurtling through space at high speed. At the George Washington University campus last week, eyes young and old were trained on the screen, witnessing an amazing story of what can happen in space.
And no, it was not “Gravity”. Nothing against Ms. Bullock or Mr. Clooney, but the 33rd International Electric Propulsion Conference was the place to be last week. The IEPC showcased some fascinating new developments in electric propulsion, including some very promising work on plasma and fusion engines. MSNW gave a great overview of their Fusion Driven Rocket, Ad Astra showed off impressive experimental results of their VASIMR engine, and the University of Surrey presented a novel quad confinement thruster, to name a few.
We were happy to present our paper on the Direct Fusion Drive Rocket for Asteroid Deflection.