Kevin L.G. Parkin

Last updated

Kevin L.G. Parkin (born 1977 in London) is an American British scientist who is best known for his study of beamed energy propulsion. [1]

Contents

Areas of interest

Rocket propulsion and gasdynamics, high power microwaves and directed energy, object-oriented software engineering, space mission design. ince 2016, Kevin has served as the systems director of Breakthrough Starshot, a $100M initiative to send a beam-driven probe to Alpha Centauri within the next generation. [2]

Education

Parkin attended the University of Leicester, where he received his bachelor's degree in physics in 1999. He then attended graduate school at the California Institute of Technology, where he received his master's degree in science in 2001. [3] He completed his Ph.D. at Caltech in 2006, from which he derived his research for beam energy. [4]

Career

Parkin was previously a member of the Carnegie Mellon Silicon Valley Research Staff [5] and previously Deputy Director of the Mission Design Center at NASA Ames, and project lead for the Microwave Thermal Rocket. [6] [3] Beginning with his Ph.D. thesis on Microwave Thermal Propulsion, his work spans theoretical, computational and experimental domains for the general problem of space access and economics. In July 2005, he was awarded the Korolev Medal by the Russian Federation of Cosmonautics. [7]

He founded the NASA Ames Mission Design Center (MDC) and developed its software architecture. The Ames MDC was the first of its kind to make extensive use of groupware, for example in pooling knowledge to create and maintain spacecraft parts databases. Another innovation was the use of a centralized parametric mission design archive that enables realtime concurrent design collaboration and object-oriented style 'inheritance' of missions to promote reuse of designs and the growth of design trees. [8]

In 2010, Parkin was tapped by the NASA Ames Center Director to manage the 100 year Starship study for NASA and DARPA. [9]

Parkin is a member of the Institute of Physics (IOP). [3]

Patents and selected publications

Related Research Articles

<span class="mw-page-title-main">Interstellar travel</span> Hypothetical travel between stars or planetary systems

Interstellar travel is the hypothetical travel of spacecraft from one star system, solitary star, or planetary system to another. Interstellar travel is expected to prove much more difficult than interplanetary spaceflight due to the vast difference in the scale of the involved distances. Whereas the distance between any two planets in the Solar System is less than 30 astronomical units (AU), stars are typically separated by hundreds of thousands of AU, causing these distances to typically be expressed instead in light-years. Because of the vastness of these distances, non-generational interstellar travel based on known physics would need to occur at a high percentage of the speed of light; even so, travel times would be long, at least decades and perhaps millennia or longer.

<span class="mw-page-title-main">Spacecraft propulsion</span> Method used to accelerate spacecraft

Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites. In-space propulsion exclusively deals with propulsion systems used in the vacuum of space and should not be confused with space launch or atmospheric entry.

<span class="mw-page-title-main">Solar sail</span> Space propulsion method using sun radiation

Solar sails are a method of spacecraft propulsion using radiation pressure exerted by sunlight on large surfaces. A number of spaceflight missions to test solar propulsion and navigation have been proposed since the 1980s. The first spacecraft to make use of the technology was IKAROS, launched in 2010.

<span class="mw-page-title-main">Ion thruster</span> Spacecraft engine that generates thrust by generating a jet of ions

An ion thruster, ion drive, or ion engine is a form of electric propulsion used for spacecraft propulsion. It creates thrust by accelerating ions using electricity.

A pulsed plasma thruster (PPT), also known as a plasma jet engine, is a form of electric spacecraft propulsion. PPTs are generally considered the simplest form of electric spacecraft propulsion and were the first form of electric propulsion to be flown in space, having flown on two Soviet probes starting in 1964. PPTs are generally flown on spacecraft with a surplus of electricity from abundantly available solar energy.

A nuclear electric rocket is a type of spacecraft propulsion system where thermal energy from a nuclear reactor is converted to electrical energy, which is used to drive an ion thruster or other electrical spacecraft propulsion technology. The nuclear electric rocket terminology is slightly inconsistent, as technically the "rocket" part of the propulsion system is non-nuclear and could also be driven by solar panels. This is in contrast with a nuclear thermal rocket, which directly uses reactor heat to add energy to a working fluid, which is then expelled out of a rocket nozzle.

Beam-powered propulsion, also known as directed energy propulsion, is a class of aircraft or spacecraft propulsion that uses energy beamed to the spacecraft from a remote power plant to provide energy. The beam is typically either a microwave or a laser beam and it is either pulsed or continuous. A continuous beam lends itself to thermal rockets, photonic thrusters and light sails, whereas a pulsed beam lends itself to ablative thrusters and pulse detonation engines.

<span class="mw-page-title-main">Variable Specific Impulse Magnetoplasma Rocket</span> Electrothermal thruster in development

The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an electrothermal thruster under development for possible use in spacecraft propulsion. It uses radio waves to ionize and heat an inert propellant, forming a plasma, then a magnetic field to confine and accelerate the expanding plasma, generating thrust. It is a plasma propulsion engine, one of several types of spacecraft electric propulsion systems.

<span class="mw-page-title-main">Starship</span> Spacecraft designed for interstellar travel

A starship, starcraft, or interstellar spacecraft is a theoretical spacecraft designed for traveling between planetary systems.

<span class="mw-page-title-main">Laser propulsion</span> Form of beam-powered propulsion

Laser propulsion is a form of beam-powered propulsion where the energy source is a remote laser system and separate from the reaction mass. This form of propulsion differs from a conventional chemical rocket where both energy and reaction mass come from the solid or liquid propellants carried on board the vehicle.

<span class="mw-page-title-main">Solar electric propulsion</span> High efficiency engine for space travel

Solar electric propulsion (SEP) refers to the combination of solar cells and electric thrusters to propel a spacecraft through outer space. This technology has been exploited in a variety of spacecraft by the European Space Agency (ESA), the JAXA, Indian Space Research Organisation (ISRO) and NASA. SEP has a significantly higher specific impulse than normal chemical rockets, thus requiring less propellant mass to be launched with a spacecraft. The technology has been evaluated for missions to Mars.

<span class="mw-page-title-main">Gridded ion thruster</span> Space propulsion system

The gridded ion thruster is a common design for ion thrusters, a highly efficient low-thrust spacecraft propulsion method running on electrical power by using high-voltage grid electrodes to accelerate ions with electrostatic forces.

<span class="mw-page-title-main">Interstellar probe</span> Space probe that can travel out of the Solar System

An interstellar probe is a space probe that has left—or is expected to leave—the Solar System and enter interstellar space, which is typically defined as the region beyond the heliopause. It also refers to probes capable of reaching other star systems.

This is an alphabetical list of articles pertaining specifically to aerospace engineering. For a broad overview of engineering, see List of engineering topics. For biographies, see List of engineers.

<span class="mw-page-title-main">Spacecraft electric propulsion</span> Type of space propulsion

Spacecraft electric propulsion is a type of spacecraft propulsion technique that uses electrostatic or electromagnetic fields to accelerate mass to high speed and thus generate thrust to modify the velocity of a spacecraft in orbit. The propulsion system is controlled by power electronics.

<span class="mw-page-title-main">Modular Common Spacecraft Bus</span> General purpose spacecraft platform

The Modular Common Spacecraft Bus (MCSB) is a fast-development, low-cost, general purpose spacecraft platform. Its modular design is intended to reduce the cost, complexity, and lead time on missions by providing a reliable, well-characterized system that can carry a variety of payloads. According to NASA, "the spacecraft is roughly one tenth the price of a conventional uncrewed mission and could be used to land on the Moon, orbit Earth, or rendezvous with near-Earth objects."

A thermal rocket is a rocket engine that uses a propellant that is externally heated before being passed through a nozzle to produce thrust, as opposed to being internally heated by a redox (combustion) reaction as in a chemical rocket.

<span class="mw-page-title-main">Nuclear power in space</span> Space exploration using nuclear energy

Nuclear power in space is the use of nuclear power in outer space, typically either small fission systems or radioactive decay for electricity or heat. Another use is for scientific observation, as in a Mössbauer spectrometer. The most common type is a radioisotope thermoelectric generator, which has been used on many space probes and on crewed lunar missions. Small fission reactors for Earth observation satellites, such as the TOPAZ nuclear reactor, have also been flown. A radioisotope heater unit is powered by radioactive decay and can keep components from becoming too cold to function, potentially over a span of decades.

<span class="mw-page-title-main">Breakthrough Starshot</span> Interstellar probe project

Breakthrough Starshot is a research and engineering project by the Breakthrough Initiatives to develop a proof-of-concept fleet of light sail interstellar probes named Starchip, to be capable of making the journey to the Alpha Centauri star system 4.37 light-years away. It was founded in 2016 by Yuri Milner, Stephen Hawking, and Mark Zuckerberg.

The future of space exploration involves both telescopic exploration and the physical exploration of space by robotic spacecraft and human spaceflight.

References

  1. "NASA Exploring Laser Beams to Zap Rockets Into Outer Space". FoxNews.com. January 13, 2015. Retrieved December 30, 2022.
  2. "Breakthrough Starshot Leaders". Breakthrough Initiatives. Retrieved December 30, 2022.
  3. 1 2 3 "About Parkin Research". Parking Research. Retrieved December 30, 2022.
  4. Parkin, Kevin L.G. (May 26, 2006). The Microwave Thermal Thruster and Its Application to the Launch Problem (Report). Caltech University. Retrieved December 30, 2022.
  5. "Kevin Parkin, Professional Research Staff Carnegie Mellon University". Archived from the original on August 24, 2011. Retrieved December 30, 2022.{{cite web}}: CS1 maint: bot: original URL status unknown (link)
  6. Turdiman, Daniel (October 20, 2010). "Rocket scientist aims to relaunch propulsion technology". CNET. Retrieved December 30, 2022.
  7. "How will we receive signals from interstellar probes like Starshot?". phys.org. May 27, 2020. Retrieved December 30, 2022.
  8. "NASA Ames Mission Design Center". NASA. Retrieved December 30, 2022.
  9. "NASA's Ames Director Announces "100 Year Starship"". Universe Today. October 20, 2010. Retrieved December 30, 2022.