Lab Capabilities

Hypergolic Propellant Handling

Streak Camera Results
Schematic of the hypergolic propellants lab (Click for details).
  • The hypergolics propellant laboratory is a dedicated facility for propellant development and fundamental combustion research
  • Dedicated ventilation system maintains lower pressure in lab than the control room
  • Three fume hoods allow for safe, separate storage and study of fuels and oxidizers as well as larger experiments
  • Positive pressure suits, PPE, and room and personal sensors allow safe experiments with harmful chemicals
  • Capability for personnel to operate equipment remotely from the control room

ROSS 2000 Streak Camera System

Streak Camera Results
Time resolved spectroscopy during a drop test of TEB/WFNA obtained with the streak camera system.
  • The ROSS 2000 streak camera is an ultrahigh-speed spectroscopic detector capable of:
    • Spectral imaging encompassing the UV and Visible ranges from 200-900 nm
    • Spectroscopic measurement at time scales applicable to hypergolic reactions
    • Sweeps over durations of 300 ns to 30 ms with a temporal resolution < 40 ps
    • Simultaneous measurements over a maximum of 180 nm wavelength range

Agilent Cary 680 FTIR Spectrometer

FTIR System
Agilent Cary 680 FTIR system with gladiATR and flow through system installed (Click image for details).
  • The Agilent Cary 680 FTIR spectrometer is capable of Fourier transform infrared spectroscopy (FTIR) of condensed and gas phase samples
    • Spectral range from 9,000-350 cm-1
    • ~110 spectra/second at 16 cm-1 resolution for kinetics experiments
    • Ventilated enclosure allows experiments with toxic materials
  • Pike GladiATR accessory
    • Diamond crystal internal reflection element enables study of corrosive condensed phase samples
    • Temperature conditioned (-40 to 100°C) ATR crystal plate
    • Liquid flow through attachment for reaction monitoring

Lambda EZ 301 Spectrometer

  • The Lambda EZ 301 Spectrometer is designed for UV/Visible spectroscopic analyses of liquid, solid, and gaseous samples
  • Absorption/transmission measurements over a specific wavelength region:
    • Grating sweep speed up to 3600 nm/min
    • 1100 to 190 nm in ~30 seconds
  • Wavelengths can be scanned repeatedly to evaluate changes with respect to time
  • Can additionally record absorbance or transmittance at a given wavelength as a function of time

LabRAM Resodyn Mixer

Resodyn LabRAM
  • The LabRAM Resodyn mixer uses acoustics for rapid and uniform mixing:
    • Consistent, complete mixing across batches without contamination of external mixing paddles
    • Enclosed mixing containers enable mixing toxic materials with minimal exposure risk
    • Rapid mixing in a variety of containers with a 500 g capacity
    • Mixes gases, liquids, solids, powders, pellets, viscous liquids, and pastes

Eppendorf 5810R Centrifuge

eppendorf Centrifuge
  • The Eppendorf 5810R Centrifuge allows for the study of particle stability
  • Configurable swing bucket rotors provide up to 4 x 750 mL capacity
  • Maximum speed of 14,000 rpm imparts over 10,000g's to samples
  • Temperature conditioned (-9 to 40°C) sample compartment

Hypergolic Droplet Characterization

Droplet Chamber
  • Configurable for single droplet or droplet impact studies
  • Controlled environment:
  • Optical accessibility to allow for multiple diagnostic techniques
    • Variable pressure up to 10 atm
    • Variable temperature up to 450 K
    • Variable chamber gas composition
    • Impact velocities up to 10 m/s

Impinging Jet System

Spray Schematic
  • Variable chamber pressure, temperature, and gas composition
  • Configurable and repeatable injection conditions
    • Variable O/F, momentum ratio, injection duration
    • Linear actuators provide ~3 ms to steady state commanded injection conditions
    • Programmable pulsed mode operation capability
  • Two combustion chamber configurations
    • 360° optically accessible, atmospheric pressure, fused silica chamber
    • 250 psia elevated pressure combustion chamber with high frequency pressure measurement
  • Measured results: Ignition delay and combustion efficiency

Laser Diagnostics

Optical Table
  • Planar Laser Induced Fluorescence (PLIF) imaging of the OH radical at up to 5 kHz
  • High frequency 3-D imaging with rotating mirror
  • Measurements on hypergolic droplet characterization and impinging jet systems

Rheometer

Capillary Rheometer
  • Rheometer allows for characterization of Non-Newtonian propellants
    • System designed for safe experimentation with toxic propellants
    • Remote operation at driving pressures up to 3000 psia
    • Controllable shear rate up to 106 1/s
  • Measured results: Propellant viscosity, storage/loss modulus, yield stress
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