Exploring the Universe with Nuclear Power

Article Updated: 23 Dec , 2015

In the past four decades, NASA and other space agencies from around the world have accomplished some amazing feats. Together, they have sent manned missions to the Moon, explored Mars, mapped Venus and Mercury, conducted surveys and captured breathtaking images of the Outer Solar System. However, looking ahead to the next generation of exploration and the more-distant frontiers that remain to be explored, it is clear that new ideas need to be put forward of how to quickly and efficiently reach those destinations.

Basically, this means finding ways to power rockets that are more fuel and cost-effective while still providing the necessary power to get crews, rovers and orbiters to their far-flung destinations. In this respect, NASA has been taking a good look at nuclear fission as a possible means of propulsion.

In fact, according to presentation made by Doctor Michael G. Houts of the NASA Marshall Space Flight Center back in October of 2014, nuclear power and propulsion have the potential to be “game changing technologies for space exploration.”

As the Marshall Space Flight Center’s manager of nuclear thermal research, Dr. Houts is well versed in the benefits it has to offer space exploration. According to the presentation he and fellow staffers made, a fission reactor can be used in a rocket design to create Nuclear Thermal Propulsion (NTP). In an NTP rocket, uranium or deuterium reactions are used to heat liquid hydrogen inside a reactor, turning it into ionized hydrogen gas (plasma), which is then channeled through a rocket nozzle to generate thrust.

NASA design for a Nuclear Engine for Rocket Vehicle Application (NERVA). Credit: NASA

NASA design for a Nuclear Engine for Rocket Vehicle Application (NERVA). Image Credit: NASA

A second possible method, known as Nuclear Electric Propulsion (NEC), involves the same basic reactor converted its heat and energy into electrical energy which then powers an electrical engine. In both cases, the rocket relies on nuclear fission to generates propulsion rather than chemical propellants, which has been the mainstay of NASA and all other space agencies to date.

Compared to this traditional form of propulsion, both NTP and NEC offers a number of advantages. The first and most obvious is the virtually unlimited energy density it offers compared to rocket fuel.  At a steady state, a fission reactor produces an average of 2.5 neutrons per reaction. However, it would only take a single neutron to cause a subsequent fission and produce a chain reaction and provide constant power.

In fact, according to the report, an NTP rocket could generate 200 kWt of power using a single kilogram of  uranium for a period of 13 years – which works out of to a fuel efficiency rating of about 45 grams per 1000 MW-hr.

In addition, a nuclear-powered engine could also provide superior thrust relative to the amount of propellant used. This is what is known as specific impulse, which is measured either in terms of kilo-newtons per second per kilogram (kN·s/kg) or in the amount of seconds the rocket can continually fire. This would cut the total amount of propellent needed, thus cutting launch weight and the cost of individual missions. And a more powerful nuclear engine would mean reduced trip times, another cost-cutting measure.

The key elements of a NERVA solid-core nuclear-thermal engine. Credit: NASA

The key elements of a NERVA solid-core nuclear-thermal engine. Credit: NASA

Although no nuclear-thermal engines have ever flown, several design concepts have been built and tested over the past few decades, and numerous concepts have been proposed. These have ranged from the traditional solid-core design to more advanced and efficient concepts that rely on either a liquid or a gas core.

In the case of a solid-core design, the only type that has ever been built, a reactor made from materials with a very high melting point houses a collection of solid uranium rods which undergo controlled fission. The hydrogen fuel is contained in a separate tank and then passes through tubes around the reactor, gaining heat and converted into plasma before being channeled through the nozzles to achieve thrust.

Using hydrogen propellant, a solid-core design typically delivers specific impulses on the order of 850 to 1000 seconds, which is about twice that of liquid hydrogen-oxygen designs – i.e. the Space Shuttle’s main engine.

However, a significant drawback arises from the fact that nuclear reactions in a solid-core model can create much higher temperatures than the conventional materials can withstand. The cracking of fuel coatings can also result from large temperature variations along the length of the rods, which taken together, sacrifices much of the engine’s potential for performance.

Diagram of an open-cycle, nuclear-thermal engine concept. Credit: NASA

Diagram of an open-cycle, gas design for a nuclear-thermal rocket engine. Credit: NASA

Many of these problems were addressed with the liquid core design, where nuclear fuel is mixed into the liquid hydrogen and allowing the fission reaction to take place in the liquid mixture itself. This design can operate at temperatures above the melting point of the nuclear fuel thanks to the fact that the container wall is actively cooled by the liquid hydrogen. It is also expected to deliver a specific impulse performance of 1300 to 1500 (1.3 to 1.5 kN·s/kg) seconds.

However, compared to the solid-core design, engines of this type are much more complicated, and therefore more expensive and difficult to build. Part of the problem has to do with the time it takes to achieve a fission reaction, which is significantly longer than the time it takes to heat the hydrogen fuel. Therefore, engines of this kind require methods to both trap the fuel inside the engine while simultaneously allowing heated plasma the ability to exit through the nozzle.

The final classification is the gas-core engine, a modification of the liquid-core design that uses rapid circulation to create a ring-shaped pocket of gaseous uranium fuel in the middle of the reactor that is surrounded by liquid hydrogen. In this case, the hydrogen fuel does not touch the reactor wall, so temperatures can be kept below the melting point of the materials used.

An engine of this kind could allow for specific impulses of 3000 to 5000 seconds (30 to 50 kN·s/kg). But in an “open-cycle” design of this kind, the losses of nuclear fuel would be difficult to control. An attempt to remedy this was drafted with the “closed cycle design” – aka. the “nuclear lightbulb” engine – where the gaseous nuclear fuel is contained in a series of super-high-temperature quarts containers.

Diagram of a closed-concept (aka. Lightbulb) gas core nuclear-thermal engine. Credit: NASA

The closed-concept (aka. Lightbulb) gas core nuclear-thermal rocket engine. Credit: NASA

Although this design is less efficient than the open-cycle design, and has a more in common with the solid-core concept, the limiting factor here is the critical temperature of quartz and not that of the fuel stack. What’s more, the closed-cycle design is expected to still deliver a respectable specific impulse of about 1500–2000 seconds (15–20 kN·s/kg).

However, as Houts indicated, one of the greatest assets nuclear fission has going for it is the long history of service it has enjoyed here on Earth. In addition to commercial reactors providing electricity all over the world, naval vessels (such as aircraft carriers and submarines) have made good use of slow-fission reactors for decades.

Also, NASA has been relying on nuclear reactors to power unmanned craft and rover for over four decades, mainly in the form of Radioisotope Thermoelectric Generators (RTGs) and Radioisotope Heater Units (RHU). In the case of the former, heat is generated by the slow decay of plutonium-238 (Pu-238), which is then converted into electricity. In the case of the latter, the heat itself is used to keep components and ship’s systems warm and running.

These types of generators have been used to power and maintain everything from the Apollo rockets to the Curiosity Rover, as well as countless satellites, orbiters and robots in between. Since its inception,a  total of 44 missions have been launched by NASA that have used either RTGs or RHUs, while the former-Soviet space program launched a comparatively solid 33.

Using modular components, a NTP spacecraft could be fitted for numerous missions profiles. Credit: NASA

Using modular components, a NTP spacecraft could be fitted for numerous missions profiles. Credit: NASA

Nuclear engines were also considered for a time as a replacement for the J-2, a liquid-fuel cryogenic rocket engine used on the S-II and S-IVB stages on the Saturn V and Saturn I rockets. But despite their being numerous versions of a solid-core reactors produced and tested in the past, none were ever put into service for an actual space flight.

Between 1959 and 1972, the United States tested twenty different sizes and designs during Project Rover and NASA’s Nuclear Engine for Rocket Vehicle Application (NERVA) program. The most powerful engine ever tested was the Phoebus 2a, which during a high-power test operated for a total of 32 minutes – 12 minutes of which were at power levels of more than 4.0 million kilowatts.

But looking to the future, Houts’ and the Marshall Space Flight Center see great potential and many possible applications. Examples cited in the report include long-range satellites that could explore the Outer Solar System and Kuiper Belt, fast, efficient transportation for manned missions throughout the Solar System, and even the provisions of power for settlements on the Moon and Mars someday.

One possibility is to equip NASA’s latest flagship – the Space Launch System (SLS) – with chemically-powered lower-stage engines and a nuclear-thermal engine on its upper stage. The nuclear engine would remain “cold” until the rocket had achieved orbit, at which point the upper stage would be deployed and reactor would be activated to generate thrust.

Credit: NASA

NASA proposals for nuclear-powered exploration rovers and craft. Credit: NASA

This concept for a “bimodal” rocket – one which relies on chemical propellants to achieve orbit and a nuclear-thermal engine for propulsion in space – could become the mainstay of NASA and other space agencies in the coming years. According to Houts and others at Marshall, the dramatic increase in efficiency offered by such rockets could also facilitate NASA’s plans to explore Mars by allowing for the reliable delivery of high-mass automated payloads in advance of manned missions.

These same rockets could then be retooled for speed (instead of mass) and used to transport the astronauts themselves to Mars in roughly half the time it would take for a conventional rocket to make the trip. This would not only save on time and cut mission costs, it would also ensure that the astronauts were exposed to less harmful solar radiation during the course of their flight.

To see this vision become reality, Dr. Houts and other researchers from the Marshall Space Center’s Propulsion Research and Development Laboratory are currently conducting NTP-related tests at the Nuclear Thermal Rocket Element Environmental Simulator (or “NTREES”) in Huntsville, Alabama.

Here, they have spent the past few years analyzing the properties of various nuclear fuels in a simulated thermal environment, hoping to learn more about how they might effect engine performance and longevity when it comes to a nuclear-thermal rocket engine.

Concept art showing a nuclear thermal propulsion piloted craft achieving Mars orbit. Credit: NASA

Concept art showing a nuclear thermal propulsion piloted craft achieving Mars orbit. Credit: NASA

These tests are slated to run until June of 2015, and are expected to lay the groundwork for large-scale ground tests and eventual full-scale testing in flight. The ultimate goal of all of this is to ensure that a manned mission to Mars takes place by the 2030s, and to provide NASA flight engineers and mission planners with all the information they need to see it through.

But of course, it is also likely to have its share of applications when it comes to future Lunar missions, sending crews to study Near-Earth Objects (NEOs), and sending craft to the Jovian moons and other locations in the outer Solar System. As the report shows, NTP craft can be easily modified using modular components to perform everything from Lunar cargo landings to crewed missions, to surveying Near-Earth Asteroids (NEAs).

The universe is a big place, and space exploration is still very much in its infancy. But if we intend to keep exploring it and reaping the rewards that such endeavors have to offer, our methods will have to mature. NTP is merely one proposed possibility. But unlike Nuclear Pulse Propulsion, the Daedalus concept, anti-matter engines, or the Alcubierre Warp Drive, a rocket that runs on nuclear fission is feasible, practical, and possible within the near-future.

Nuclear thermal research at the Marshall Center is part of NASA’s Advanced Exploration Systems (AES) Division, managed by the Human Exploration and Operations Mission Directorate and including participation by the U.S. Department of Energy.

Further Reading: NASA, NASA NTRS

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21 Responses

  1. Beckler says

    “…nuclear power and propulsion have the potential to be “game changing technologies for space exploration.”

    Reading this you’d think nuclear energy is some amazing new discovery. If we’d put more money into this instead of blowing it all on nuclear weapons and hyper-massive military infrastructure, nuclear engines could’ve been around 30 years ago instead of still being 30 years away.

    • choklit says

      But it was the need for powerful rockets to launch nuclear weapons around the world that was the original reason to fund nuclear rocket research in the first place. Without that impetus it would still be a figment of nuclear engineer’s imaginations.

  2. dimar says

    Still nothing on fusion power?

  3. FarAwayLongAgo says

    I’ve read some sober people who explain that there’s actually not enough demand for nuclear power in space yet. It would not be economical to develop nuclear propulsion for only one mission to the outer Solar system per decade. Nuclear thermal propulsion scales very well, but with today’s lowly space programs it would not be the panacea. Nuclear is a bit too big for the pocket sized space flight we have today. If we invested ten times as much in space, then nuclear would be the way to go. But it doesn’t seem to be worthwhile for the ISS or a single rover or a small Pluto flyby mission.

    • choklit says

      Yeah. The problem is that there is no mission that would require the use of NTR. I love NTR. I would love nothing more than to see it live again and fly. But right now it is a distraction. The focus needs to be getting a real mission for human space flight with mostly current technology that is worth the money spent, the risk taken and benefits overall human space exploration. I think Constellation was the right step. I like Mars Direct, too. As has happened many, many times in the past, if we focus on developing technology first without a real mission directive, it will be cancelled in subsequent budgets and human exploration missions will be pushed back another decade. That’s just the way it works. If we go back o the moon and establish a base, or execute Mars Direct, then it will be time to start demanding this kind of thing.

  4. philw1776 says

    THIS is what NASA should be doing in its spaceflight R&D money. Not the boondoggle SLS which even when and if it flies will be too expensive to fly. Let NASA develop the controversial nuclear technology and fly it on Falcon Heavy or better yet the SpaceX BFR next decade. Really large payloads to the outer planets would enable multiple landers and orbiters around Europa, Enceladus and Titan and even Triton.

    Nukes for Mars transit & return would allow within opposition full return trips and larger payloads for Musk’s Mars initiative.

    • Patreon
      Aqua4U says

      Ahem… “One possibility is to equip NASA’s latest flagship – the Space Launch System (SLS) – with chemically-powered lower-stage engines and a nuclear-thermal engine on its upper stage. The nuclear engine would remain “cold” until the rocket had achieved orbit, at which point the upper stage would be deployed and reactor would be activated to generate thrust.”

      Yes.. a properly shielded human rated NTP reactor will no doubt be pretty heavy and will require lots of thrust to launch… aka use of the SLS 1st stage booster to LEO.

  5. Jason says

    Generating clean, safe and dense energy in space, with no risk of radiation damage to the crewmembers, is a key problem for space voyages. A fission nuclear reactor in space needs massive radiators to get rid of waste heat. At least two-thirds of the energy generated is wasted as heat, but using a more efficient thermoelectric converter it is possible to recover most of the thermal energy into electricity. http://youtu.be/u8n7j5k-_G8

  6. Feenixx says

    I would like to believe long term plans for nuclear power development are perhaps dated – instead, we are looking at down-scaled fusion power quite soon … most definitely Lockheed Martin’s Compact Fusion, but there are others ….

    • choklit says

      It would be nice if Lockheed bothered to publish a scientific paper to back their announcement. Without that there is no way to verify that what they said is not just hype. The best not-big-government project for fusion out there is EMC2 Corp. Their lead scientist, Jaeyoung Park, just spoke at Microsoft Research and his progress, following the work started by Robert Bussard, is the best place to focus.

  7. UFOsMOTHER says

    I agree with the comment made by Far Away Long Ago for this time in history, But in the distant future when and if we ever decide to leave our solar system and aim for the stars it could be an option….

  8. Patreon
    Aqua4U says

    Well written and informative.. good job. Can you tell that I am a proponent? I lean more toward using a reactor to generate electricity via MHD over systems that eject spent radioactive fuel. A moderately sized reactor could produce around 700 MWe? Use that to power a super VASIMR engine(s) AND create a powerful magnetic bubble around the crew to shunt charged particles? Lets GO!


    • choklit says

      The VASIMR concept is a far off idea; it will not send humans anywhere anytime soon. If you want to go somewhere in the near future with nuclear power, NTR is a far better choice. VASIMR is one of many technology projects that NASA is told to showcase to make it look like they are doing something while the true purpose is to keep NASA on hold. It’s especially infuriating since they are spending pretty much the same amount of money every year, but the powers that be clearly do not want NASA doing high profile human space missions. Maybe the next administration will feel differently.

  9. On the subject of nuclear, I wonder just how hard it would be to detect a nuclear burst on a distant planet, like that of Hiroshima or Nagasaki. That would be one way of proving the existence of extraterrestrials . . . or maybe I should say the former existence.

  10. Planetwatcher says

    Using nuclear fission for space propulsion would need a much bigger market then we currently have. However, holding out for the distant future, makes pretty much no since, and likewise trying to use fission propulsion for interstellar missions, or even to the outer reaches of the Ort Cloud is completely futile. However, it is idea for use within the middle and outer solar system, and the Kuiper Belt, where years and decades of travel using conventional rockets could be reduced to more manageable weeks, or months.
    The unavoidable issue is how to protect human space travelers from radiation. Current nuclear power plants use walls of concrete over 8 feet thick, and other buildings surrounding the reactor building to protect humans. This is not practical in space. If and when a means of protecting humans from fission’s radiation is found, and made accessible, we will then have a very very good source of power, and propulsion for anywhere in the Solar system.

  11. GREverett says

    By treaty no nuclear pile can go critical in earth orbit. Accordingly, it is more likely that any reactor section would have to be modular and tugged out to L1 or L2 for assembly with the other components of the deep space exploration vessel (doesn’t that sound good “deep space exploration vessel”). Also, since it is likely that a fission design would at some point be superseded by a fusion design. It makes more since to develop a plasma engine (ala VASIMR) or a Fission Fragment engine (also a Marshal product), which have some technical commonality with fusion systems. The development of a modernized NTR would be a big expensive project. If we are going to do a big expensive project, let it not be something that doesn’t lead anywhere.

    • What about nuclear subs and the lead containment they use? That’s an existing solution, though adapting to a rocket design would present engineering and technical challenges for sure.

  12. LoboSolo says

    The TRITON was set forth a long time ago … I think as a follow-on to NERVA. http://www.alternatewars.com/BBOW/Space_Engines/AIAA-2004-3863_TRITON.pdf

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