Japan Geoscience Union Meeting 2023

Presentation information

[E] Online Poster

P (Space and Planetary Sciences ) » P-PS Planetary Sciences

[P-PS01] Outer Solar System Exploration Today, and Tomorrow

Thu. May 25, 2023 3:30 PM - 5:00 PM Online Poster Zoom Room (1) (Online Poster)

convener:Jun Kimura(Osaka University), Kunio M. Sayanagi(NASA Langley Research Center ), Fuminori Tsuchiya(Planetary Plasma and Atmospheric Research Center, Graduate School of Science, Tohoku University)

On-site poster schedule(2023/5/25 17:15-18:45)

3:30 PM - 5:00 PM

[PPS01-P04] The Ganymede Laser Altimeter (GALA) for the Jupiter Icy Moons Explorer (JUICE): Performance Model Simulation

*Hiroshi Araki1, Ishibashi Ko2, Noriyuki Namiki1, Hirotomo Noda1, Masanori Kobayashi2, Keigo Enya3, Masanobu Ozaki1, Mizuno Takahide3, Yoshihumi Saito3, Kazuyuki Touhara3, Shoko Oshigami3, Shingo Kashima1, Jun Kimura4, Gregor Steinbrugge5, Alexander Stark5, Christian Althaus5, Simone Del Togno5, Kay Lingenauber5, Hauke Hussmann5 (1.National Astronomical Observatory of Japan, 2.Chiba Institute of Technology Planetary Exploration Research Center, 3.Institute of Space and Astronautical Science, 4.Osaka University, 5.German Aerospace Center)

Keywords:JUICE, GALA, laser altimeter, APD, matched filter, radiation

GALA (GAnymede Laser Altimeter) is one of the payload instruments of the JUICE (JUpiter ICy moons Explorer) to be launched in 2023 to the Jovian icy moons, Ganymede, Europa, and Callisto. GALA is developed by the international collaboration of Germany, Japan, Switzerland, and Spain.
With the GALA performance model, we searched the interface conditions that satisfy the science requirements on the probability of false detection (PFD) and the range accuracy.
The science requirements on GALA performance can be summarized as following four criteria: [A] for Europa fly-by, PFD is less than 0.2 from an altitude of 1300 km or lower, [B] under the worst observation condition for albedo and surface slope of GCO500 (Ganymede Circular Orbit whose height is 500km), the accuracy of ranging is less than 10 m and PFD is less than 0.2, [C] under the nominal observation condition of GCO500, the accuracy of ranging is less than 2 m and PFD is less than 0.1, and [D] under the best observation condition of GCO500, the accuracy of ranging is less than 1 m and PFD is less than 0.1. The minimum SNR (R_SNR) which satisfies each requirement from [A] to [D] is summarized in Table 1 through the simulation of output signal of the GALA matched filter, where the range accuracy for [A] is assumed to be ‘< 10m’. R_SNR should be less than C_SNR which is evaluated by our GALA performance model for each criterion.
For the assessment, however, we must use data for the characteristics of the laser detector of GALA, avalanche photodiode (APD) degraded due to the severe radiation environment around Jupiter. Now, we carried out realistic model simulation using GALA performance model with these degradation effects of APD. Characteristics of APD, such as gain, quantum efficiency, excess noise index, surface dark current, and bulk dark current, were re-evaluated through radiation tests using the data of dark and photo current of the APD irradiated with 2-MeV-electron and 50-MeV-proton beams, which are considered to be equivalently severe on the APD as in the radiation condition of JUICE-GALA around Jupiter.
These degraded characteristics of APD by radiation were introduced to our performance model of GALA. As a result, our performance simulation of GALA showed that the science requirements (R_SNR < C_SNR) are satisfied even after considering the degraded characteristics of APD (Table 1).