Abstract

Abstract. Characterising the photoelectron current induced by the Sun's UV radiation is crucial to ensure accurate daylight measurements from particle detectors. This article lays out the methodology used to address this problem in the case of the meteoric smoke particle detectors (MSPDs), developed by the Leibniz Institute of Atmospheric Physics in Kühlungsborn (IAP) and flown on board the PMWEs (Polar Mesosphere Winter Echoes) sounding rockets in April 2018. The methodology focuses on two complementary aspects: modelling and experimental measurements. A detailed model of the MSPD photocurrent was created based on the expected solar UV flux, the atmospheric UV absorption as a function of height by molecular oxygen and ozone, the photoelectric yield of the material coating the MSPD as a function of wavelength, the index of refraction of these materials as a function of wavelength and the angle of incidence of the illumination onto the MSPD. Due to its complex structure, composed of a central electrode shielded by two concentric grids, extensive ray-tracing calculations were conducted to obtain the incidence angles of the illumination on the central electrode, and this was done for various orientations of the MSPD in respect to the Sun. Results of the modelled photocurrent at different heights and for different materials, as well as for different orientations of the detector, are presented. As a pre-flight confirmation, the model was used to reproduce the experimental measurements conducted by Robertson et al. (2014) and agrees within an order of magnitude. An experimental setup for the calibration of the MSPD photocurrent is also presented. The photocurrent induced by the Lyman-alpha line from a deuterium lamp was recorded inside a vacuum chamber using a narrowband filter, while a UV-sensitive photodiode was used to monitor the UV flux. These measurements were compared with the model prediction, and also matched within an order of magnitude. Although precisely modelling the photocurrent is a challenging task, this article quantitatively improved the understanding of the photocurrent on the MSPD and discusses possible strategies to untangle the meteoric smoke particles (MSPs) current from the photocurrent recorded in-flight.

Highlights

  • Meteoric smoke particles (MSPs, sometimes referred to as meteor smoke particles) play an important role in the mesosphere/lower thermosphere (MLT) region

  • These meteoric smoke particles (MSPs) detectors will be part of a sounding rocket campaign aiming at investigating Polar Mesospheric Winter Echoes (PMWEs), with the first two launches conducted in April 2018 from Andøya, Norway, and two additional flights scheduled for 2019

  • A dual and complementary approach to the problem was presented by means of both modelling and experimental measurements in the particular case of a rocketborne meteoric smoke particle detector (MSPD) currently developed at the Institute of Atmospheric Physics (IAP)

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Summary

Introduction

Meteoric smoke particles (MSPs, sometimes referred to as meteor smoke particles) play an important role in the mesosphere/lower thermosphere (MLT) region. Havnes et al, 1996; Rapp and Strelnikova, 2009) These instruments are drastically affected by the aerodynamics of the rocket flight, prohibiting detection of the smallest particles, normally below 1 nm size The geometry was optimised to reduce aerodynamic and bow-shock effects, as these effects directly determine the minimum mass required for the MSPs to reach the central electrode, affecting the estimation of the MSP density These MSP detectors will be part of a sounding rocket campaign aiming at investigating PMWEs, with the first two launches conducted in April 2018 from Andøya, Norway, and two additional flights scheduled for 2019. Giono et al.: Photocurrent modelling and experimental confirmation for meteoric smoke particle detectors 5301

Ultraviolet spectral flux as a function of altitude
Material properties
Illumination on the detector
Resulting photocurrent
Comparison photocurrent measurements from a sounding rocket flight
Overview of the experiment and apparatus
Experimental measurements
Comparison with modelling
Conclusions
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