Abstract
Project New Orion entails a pulsed nuclear space propulsion system that utilizes photofission through the implementation of an ultra-intense laser. The historical origins derive from the endeavors of Project Orion, which utilized thermonuclear devices to impart a considerable velocity increment on the respective spacecraft. The shear magnitude of Project Orion significantly detracts from the likelihood of progressive research development testing and evaluation. Project New Orion incorporates a more feasible pathway for the progressive research development testing and evaluation of the pulsed nuclear space propulsion system. Photofission through the application of an ultra-intense laser enables a much more controllable and scalable nuclear yield. The energy source for the ultra-intense laser is derived from a first stage liquid hydrogen and liquid oxygen chemical propulsion system. A portion of the thermal/kinetic energy of the rocket propulsive fluid is converted to electrical energy through a magneto-hydrodynamic generator with cryogenic propellant densification for facilitating the integral superconducting magnets. Fundamental analysis of Project New Orion demonstrates the capacity to impart a meaningful velocity increment through ultra-intense laser derived photofission on a small spacecraft.
Highlights
Non-chemical space propulsion offers inherent advantages from a performance perspective with a highly economical means of imparting a considerable velocity increment on the respective spacecraft
Project New Orion offers a feasible pathway for the progressive research, test, and evaluation of pulsed nuclear propulsion configurations
The historical origins stem from the efforts of Project Orion, which advocated the use of thermonuclear devices for providing a substantial velocity increment to a respective spacecraft
Summary
Non-chemical space propulsion offers inherent advantages from a performance perspective with a highly economical means of imparting a considerable velocity increment on the respective spacecraft. Antimatter and photofission pulsed space propulsion configurations have been proposed and conceptualized by LeMoyne and Mastroianni. (2016) Project New Orion: Pulsed Nuclear Space Propulsion Using Photofission Activated by Ultra-Intense Laser. The antimatter and photofission pulsed space propulsion systems using an ultra-intense laser system incorporated a thermal energy threshold pulsed space propulsion configuration. The activation through an ultra-intense laser system enables a decoupling between the location of the propulsion system and laser energy source [1] [2] Another type of pulsed space propulsion incorporates a thermonuclear denotation. Instead of utilizing a large magnitude thermonuclear detonation to provide a velocity increment, photofission by means of an ultra-intense laser is applied. The propulsive velocity increment is derived from a photofission event based on activation from an ultra-intense laser. With the Project New Orion conceptual architecture elucidated, the objective is to demonstrate the fundamental performance analysis of Project New Orion
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