Energy Conversion in Laser Propulsion III

Abstract

Conversion of pulses of CO2 laser energy (18 microsecond pulses) to propellant kinetic energy was studied in a Myrabo Laser Lightcraft (MLL) operating with laser heated STP air and laser ablated delrin propellants. The MLL incorporates an inverted parabolic reflector that focuses laser energy into a toroidal volume where it is absorbed by a unit of propellant mass that is subsequently expanded in the geometry of the plug nozzle aerospike. With Delrin propellant, measurements of the coupling coefficients and the ablated mass as a function of laser pulse energy showed that the efficiency of conversion of laser energy to propellant kinetic energy was ^54%. With STP air, direct experimental measurement of efficiency was not possible because the propellant mass associated with measured coupling coefficients was not known. Thermodynamics predicted that the upper limit of the efficiency of conversion of the internal energy of laser heated air to jet kinetic energy, alpha, is ^0.30 for EQUILIBRIUM expansion to 1 bar pressure. For FROZEN expansion alpha ^0.27. These upper limit efficiencies are nearly independent of the initial specific energy from 1 to 110 MJ/kg. With heating of air at its Mach 5 stagnation density (5.9 kg/m3 as compared to STP air density of 1.18kg/m3) these efficiencies increase to about 0.55 (equilibrium) and 0.45 (frozen). Optimum blowdown from 1.18 kg/m3 to 1 bar occurs with expansion ratios ^1.5 to 4 as internal energy increases from 1 to 100 MJ/kg. Optimum expansion from the higher density state requires larger expansion ratios, 8 to 32. Expansion of laser ablated Delrin propellant appears to convert the absorbed laser energy more efficiently to jet kinetic energy because the effective density of the ablated gaseous Delrin is significantly greater than that of STP air.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 2002
Accession Number
ADA410650

Entities

People

  • Carl William Larson
  • F. B. Mead Jr.
  • Wayne M. Kalliomaa

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Chemical Equilibrium
  • Coefficients
  • Computer Programs
  • Energy
  • Energy Conversion
  • Equations
  • Heat Capacity
  • Kinetic Energy
  • Low Earth Orbits
  • Measurement
  • Propulsion Systems
  • Rocket Propulsion
  • Specific Heat
  • Thermodynamic Properties
  • Thermodynamics
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Combustion science or combustion engineering.
  • Pulsed Power and Plasma Physics.

Technology Areas

  • Directed Energy
  • Directed Energy - Lasers