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Guest: Dr. Jason Cassibry. Topics: A technical description and the potential of fusion propulsion. You are invited to comment, ask questions, and discuss the Space Show program/guest(s) on the Space Show blog, http://thespaceshow.wordpress.com. Comments, questions, and any discussion must be relevant and applicable to Space Show programming. Transcripts of Space Show programs are not permitted without prior written consent from The Space Show (even if for personal use) & are a violation of the Space Show copyright. We welcomed Dr. Jason Cassibry to the program to guide us in our discussion of the potential for fusion propulsion. At times, this was a very technical discussion. To assist in following it, I have uploaded to the blog his published paper delivered at the AIAA Joint Propulsion Conference, "The Case and Development Path for Fusion Propulsion." In addition, below are the URLs for several articles on fusion propulsion that Dr. Cassibry shared with us: www.uah.edu/news/items/10-research/2501-slapshot-to-deep-space#.UDrKn-iP... www.popularmechanics.com/science/space/rockets/the-big-machine-that-coul... http://io9.com/5921673/nuclear-slapshots-could-propel-a-spacecraft-to-ma... www.centauri-dreams.org/?p=23442 and http://nextbigfuture.com/2012/10/zpinch-nuclear-fusion-pulse-space.html. Dr. Cassibry started out by providing us with a working definition of fusion propulsion. We talked about nuclear propulsion as well and the overall state of development for fusion energy. I asked Dr. Cassibry if in their economic projections for fusion propulsion, they considered the political and policy impact on fossil fuel pricing and supply availability. As you will hear, generally such factors are not included in their studies though he concurred with me that such policies can strongly skew the economics one way or the other. Several calls came in on a wide ranging group of associated topics. We talked about the main fusion fuel, lithium deuteride, magnetic nozzles, and the use of a nuclear fission reactor to start the fusion propulsion unit. Z-Pinch technologies were defined and discussed. As the segment drew to a close, I asked about funding sources for this research and we learned that most all of the funding is from public sources. In our second segment, more listeners called in regarding insitu resource usage, nuclear propulsion to start the fusion unit, and the power consumed for all of this. We talked about using fusion propulsion for a Mars mission and what it did for travel times. Jason also put forth a suggested time line and path to follow to operation in perhaps 25 years, depending on funding. More calls came in with fuel questions, vibration impact, G force acceleration, thrust, and more. Another topic discussed was fusion propulsion for the launch vehicle. We then compared some real mission travel times such as Cassini, Voyager, and New Horizons, asking what the transit times would have been like using fusion propulsion. As we were ending the program, I asked about the students entering aerospace engineering at UAH, both the undergrad and graduate level, plus the gender mix of the students. There appears to be strong demand by the students to study these fields at all levels. In conclusion, Jason suggested that we could look for breakeven with fusion in about ten years, maybe less. If you have comments/questions, please post them on The Space Show blog. Dr. Cassibry's faculty page at UAH is www.mae.uah.edu/faculty/cassibry.shtml.