Abstract
The laser- and pressure-driven thrust response functions of HMX (cyclotetramethylene tetranitramine) at pressures near 1 atm were measured during laser-supported combustion at mean CO2 laser heat fluxes of 35 and 60 W/cm2. During laser-driven testing, the laser flux was modulated at ±15 W/cm2 at driving frequencies ranging from 4 to 250 Hz. Pressure-driven thrust measurements were made with a 10% peak-to-peak variation about the mean chamber pressure at driving frequencies ranging from 4 to 100 Hz. Measured steady-state temperature profiles and numerical predictions of the temperature profiles in the gas-phase reaction zone were used to estimate steady and unsteady heat feedback, respectively. Trends in the experimental results are consistent with a condensed-phase response to the unsteady heat fluxes and with results in the literature from similar experiments. Differences in trends with changing mean heat flux between the laser- and pressure-driven results are explained using the unsteady heat feedback estimates. The experimental results are compared to an analytical model, which used one-step reactions in the condensed phase and gas phase, and numerical modeling results that used detailed gas-phase chemistry. The agreement between the analytical model and the data was found to be better than that between the numerical modeling results and the data.
Original language | English (US) |
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Pages (from-to) | 1218-1226 |
Number of pages | 9 |
Journal | Journal of Propulsion and Power |
Volume | 18 |
Issue number | 6 |
DOIs | |
State | Published - 2002 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Fuel Technology
- Mechanical Engineering
- Space and Planetary Science