2016
DOI: 10.1007/978-3-319-27748-6_1
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An Introduction to Energetic Materials for Propulsion

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Cited by 21 publications
(20 citation statements)
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“…Transient IR (pump–probe) spectra and time-resolved 2D IR spectra of HHTT solvated in DMSO and in microcrystal form were collected with a pulse-shaper based 2D IR spectrometer using a germanium acousto-optic modulator (AOM) . Experimental details have been previously described. ,, A commercial femtosecond (fs) regenerative Ti:sapphire laser amplifier was used to generate laser pulses with 25 fs pulse width, 3 mJ pulse energy, and 800 nm output wavelength. Then, the 800 nm laser pulse went through an optical parametric amplifier, and a difference frequency generator, and finally produced a ∼10 μJ mid-IR pulse at 6.3 μm central wavelength.…”
Section: Methodsmentioning
confidence: 99%
“…Transient IR (pump–probe) spectra and time-resolved 2D IR spectra of HHTT solvated in DMSO and in microcrystal form were collected with a pulse-shaper based 2D IR spectrometer using a germanium acousto-optic modulator (AOM) . Experimental details have been previously described. ,, A commercial femtosecond (fs) regenerative Ti:sapphire laser amplifier was used to generate laser pulses with 25 fs pulse width, 3 mJ pulse energy, and 800 nm output wavelength. Then, the 800 nm laser pulse went through an optical parametric amplifier, and a difference frequency generator, and finally produced a ∼10 μJ mid-IR pulse at 6.3 μm central wavelength.…”
Section: Methodsmentioning
confidence: 99%
“…[9][10][11][12][13] Although this results in an increase in the specific impulse (I sp ), implementation of HECs is limited due to the increased hazard that the high-energy explosive additives bring with them, since they are impact and friction sensitive additives. [9][10][11][12][13] It has been reported in the literature, that computational results for TKX-50-based solid rocket propellant formulations (22 % energetic binder, 20 % oxidizer, 18 % Al, 40 % TKX-50) indicated that TKX-50 shows a higher density impulse than HMX, but is lower than that of CL-20. [14] The NASA SP-273 computer code was used to predict the parameters of rocket propellant formulations, and was able to show that TKX-50 containing formulations showed a superior specific impulse value compared to corresponding formulations in which TKX-50 was replaced by other common explosives.…”
mentioning
confidence: 99%
“…Recently, many studies have focused on obtaining new oxidizing agents, by synthesis of novel compounds or modification of known compounds. The aim was to obtain compounds that meet the current requirements for solid rocket fuels (non-polluting, characterized by a good oxygen balance and providing high specific impulse) [41][42][43].…”
Section: Novel Oxidizing Agentsmentioning
confidence: 99%