Characterization of Ammonia Borane for Chemical Propulsion Applications
Open Access
- Author:
- Weismiller, Michael Raymond
- Graduate Program:
- Mechanical Engineering
- Degree:
- Doctor of Philosophy
- Document Type:
- Dissertation
- Date of Defense:
- May 25, 2012
- Committee Members:
- Richard A Yetter, Dissertation Advisor/Co-Advisor
Richard A Yetter, Committee Chair/Co-Chair
Prof Adrianus Van Duin, Committee Member
Stefan Thynell, Committee Member
Randy Lee Vander Wal, Committee Chair/Co-Chair - Keywords:
- Energetic materials
Novel propellants
Hydrogen storage
Hybrid rocket
Boron - Abstract:
- Ammonia borane (NH3BH3; AB), which has a hydrogen content of 19.6% by weight, has been studied recently as a potential means of hydrogen storage for use in fuel cell applications. Its gaseous decomposition products have a very low molecular weight, which makes AB attractive in a propulsion application, since specific impulse is inversely related to the molecular weight of the products. AB also contains boron, which is a fuel of interest for solid propellants because of its high energy density per unit volume. Although boron particles are difficult to ignite due to their passivation layer, the boron molecularly bound in AB may react more readily. The concept of fuel depots in low-earth orbit has been proposed for use in deep space exploration. These would require propellants that are easily storable for long periods of time. AB is a solid at standard temperature and pressure and would not suffer from mass loss due to boil-off like cryogenic hydrogen. The goal of this work is to evaluate AB as a viable fuel in chemical propulsion. Many studies have examined AB decomposition at slow heating rates, but in a propellant, AB will experience rapid heating. Since heating rate has been shown to affect the thermolysis pathways in energetic materials, AB thermolysis was studied at high heating rates using molecular dynamics simulations with a ReaxFF reactive force field and experimental studies with a confined rapid thermolysis set-up using time-of-flight mass spectrometry and FTIR absorption spectroscopy diagnostics. Experimental results showed the formation of NH3, H2NBH2, H2, and at later times, c-(N3B3H6) in the gas phase, while polymer formation was observed in the condensed phase. Molecular dynamics simulations provided an atomistic description of the reactions which likely form these compounds. Another subject which required investigation was the reaction of AB in oxidizing environments, as there were no previous studies in the literature. Oxygen bond descriptions were added to the ReaxFF force field and molecular dynamics simulations were performed to identify important species and reactions in the AB oxidation. Since the thermodynamic properties of many of these species were unknown, density functional theory (DFT) calculations were performed in the Jaguear 7.8 program using the B3LYP functional and 6-311G**++ basis set to calculate enthalpy and entropy of formation, as well as specific heat as a function of temperature. These results were used to create a gas-phase chemical kinetic mechanism for AB combustion. New elementary reactions (57) were combined with those found in the literature for ammonia and boron oxidation, to form a mechanism of 201 reversible reactions. Results from a simple homogenous, constant pressure and energy calculation are presented in this work. The results show that H2NBH2 can be dehydrogenated via radical attack when temperatures are too low to overcome the hydrogen elimination barrier and pressures are low enough to allow sufficient radicals to form. Molecular dynamics calculations require very high pressures to facilitate reactions over a short simulation time, and show the formation of heavy B/N/H/O molecules, such as HNBOH and H2NB(OH)2. On the other hand, the chemical kinetics calculations at 1 atm show that if the HNBO molecule is further oxidized, the products will likely fission with B-N bond cleavage. The final objective towards the research goal was to study how AB can be effectively integrated into a propulsion application. AB was added to a paraffin wax binder to form a heterogeneous solid fuel matrix. Opposed-flow burner experiments were performed where a flow of gaseous oxygen was impinged on the solid fuel surface and regression rates were measured. Regression rates were shown to increase with small additions of AB, but the condensed phase product build-up at higher AB concentrations limited the solid fuel regression. Solid fuel grains with various amounts of AB were manufactured and tested in a lab scale hybrid rocket engine, where performance parameters such as thrust, chamber pressure, specific impulse (Isp) and characteristic exhaust velocity (C*), were measured. AB addition was shown to increase Isp and C*, but large additions were shown to reduce the overall thrust due to the hindrance of the solid fuel regression.