Operation principles of hypervelocity impacts of ice grains.
Dust impacts on the compositional analyzer target of the Cosmic Dust Analyzer and generated signals.
Impact ionization of ice grains is used to explore the subsurface oceans of Enceladus with the Cosmic Dust Analyzer onboard Cassini, and Europa with the SUrface Dust Analyzer (SUDA) on Europa Clipper. Impact ionization of ice grains occurs by hypervelocity (velocities > 1km/s) impacts of ice grain into a detector, during which a fraction of the ice particle is converted into elemental and molecular ions that can then be analyzed by mass spectrometry. With increasing impact speeds, the greater energy available results in the generation of more ions, the breakup of molecular ions into elemental ions, and a reduction in the amount of cluster formation, but these effects are complex and compositionally dependent. Simulating hypervelocity ice grain impacts onto space detectors is crucial for interpreting the results of ongoing and future space missions. Laboratory analogue experiments are an essential element of the quantitative interpretation of impact ionization mass spectra recorded in space. For mineral, metallic and/or organic dust particles, this can be achieved by electrostatic acceleration of micrometer and sub-micrometer sized grains, by firing them upon duplicates of the space detector. Our research group participates in such experiments at accelerator facilities in Germany (at Stuttgart University) and the USA (at the University of Colorado at Boulder).
However, such experiments are technically much harder to perform with water-rich ice grains and acceleration of icy particles to the desired speed is currently not possible. Therefore, a laser-based analogue technique has been implemented to simulate the impacts of water-rich ice grains onto impact ionization mass spectrometers.This technique uses the principle of Laser Induced Liquid Beam Ion Desorption (LILBID) coupled to a reflection time-of-flight mass spectrometer. In the LILBID process, a pulsed infrared laser intersects a micrometer-scale water beam (or similarly sized water droplets) of known composition, to simulate an ice grain impact. The laser acts onto the liquid in the same way as a mechanical hit. Energy from the laser creates a cloud of cations, anions, electrons and neutral molecules which is similar to the impact cloud created by a hypervelocity ice grain impact in space. The cations or anions are then directed into a Time-of-Flight mass spectrometer which, after a predefined delay time, generates and records the analogue mass spectra. By setting a delay time, we select ions with specific ranges of velocities. By combining different delay times with variable laser energies, we can mimic spectra generated by different speed impacts in space. The laboratory laser apparatus is therefore key for the compositional analysis of ice grains detected in space, and has proved itself invaluable for interpreting Cassini Cosmic Dust Analyzer spectra from the Saturnian system. It will be crucial for the interpretation of SUDA impact mass spectra at Europa, and future missions to Enceladus and other icy ocean moons. The recorded spectra are stored in a comprehensive spectral reference library from a wide variety of organic and inorganic analogue materials, in matrix solutions which simulate a range of icy grain bulk compositions.
Recently, the unique coupling of an Orbitrap-based mass analyzer, OLYMPIA, to the LILBID technique has been achieved in our laboratory in Berlin and as part as a collaboration with the Université d'Orléans. OLYMPIA (Orbitrap anaLYser MultiPle IonisAtion) is an instrument based on the Orbitrap analyzer that can operate with several ionization techniques, including electron impact ionization, laser ablation/desorption and Laser-Induced Liquid Beam Ion Desorption (LILBID). Although OLYMPIA is not intended to be developed as a flight instrument, it serves as a test bench to evaluate possible designs for future space-qualified instruments, supporting the development of the space instruments based on the Orbitrap.
The Orbitrap cell is a small (diameter of 30 mm) mass analyzer formed by 4 electrodes: a spindle-shaped central electrode, two external electrodes, and a deflection electrode. When applying a high voltage to the central electrode, an electric field traps ions in orbits around the central electrode. The ions oscillate back and forth, and the external electrodes detect the image current generated in this motion.
The Orbitrap anaLYzer MultiPle IonizAtion (OLYMPIA) coupled to the laser desorption LILBID technique (Left). Trajectory of the ion beam entering the Orbitrap cell (Right)
The deflection electrode directs the ion beam into the Orbitrap cell and corrects disturbances caused by the entry aperture. These oscillations of the ions are dependent on their mass, and therefore, we can record them over time, and after applying a Fourier transform and treating the data, obtain high resolution and high mass accuracy spectra. While the time-of-flight mass analyzer has a limited mass resolution (∼800 m/Δm), the Orbitrap analyzer has an unprecedented high mass resolution of up to 150 000 m/Δm. Because of its small size and unprecedented mass resolution, it is an attractive candidate for space exploration missions.
OLYMPIA has proven to be highly versatile. Our current research focuses on producing analogue spectra comparable to those from the Cosmic Dust Analyzer, by generating water clusters from liquid samples to simulate low-velocity ice grain impacts. These data will help expand the SUDA database with high-resolution spectra.
Comparison of the impact ionization process occurring in mass spectrometers in space (A) and in liquid beam laser desorption (B) for comparable energy impact and dispersion conditions. In A) ice grains hit a metal target and become partially ionized. In B) a pulsed infrared laser hits a water beam, which disperses and in turn creates ions and charged aggregates. In both cases the charged ions/aggregates are accelerated by a high voltage potential difference (neg./pos. HV) and detected after a characteristic (mass/charge dependent) time of flight. The lower panel (C) shows the main acceleration and drift zones within the CDA Chemical Analyzer mass spectrometer. Voltages are approximate and the regions are not to scale. Instrument recording may be triggered by charges exceeding thresholds on the target, acceleration grids or multiplier.
The Laser Induced Liquid Beam Ion Desorption (LILBID) facility for simulating hypervelocity impacts of ice grains onto space-based impact ionization mass spectrometers and (inset) a schematic illustrating the instrument configuration underlying the principle of delayed extraction.
The LILBID laboratory is situated on the GeoCampus in Berlin-Lankwitz, building B, 2nd floor, room B238 (phone +49 30 838 70537).
Dr. Jon Hillier (phone +49 30 838 70822, j.hillier@fu-berlin.de)
Dr. Maryse Napoleoni (phone +49 30 838 72119; m.napoleoni@fu-berlin.de)
Rene Reviol (phone +49 30 838 65473; r.reviol@fu-berlin.de)