Session
Session I: Beyond LEO
Abstract
This presentation is the product of a nine-month mission concept study for a CubeSat that would be carried aboard the JPL Europa Multiple-Flyby Mission, released in the Jovian system and make measurements at Europa. We examined the scientific return as well as the technical feasibility of a CubeSat designed to study the linkage between Europa's radiation environment which generates Europa's atmosphere through sputtering and radiolytic processes, and its atmospheric structure. This would be accomplished by measuring a) energetic particles at Europa and b) its atmospheric density through drag forces on the CubeSat. The findings of our concept study for the Deployable Atmospheric Reconnaissance CubeSat with Sputtering Ion Detector at Europa (DARCSIDE) indicate that the technology exists to enable a 3U, 4.4 kg CubeSat to detect Europa's tenuous atmosphere beginning ~200 km above the surface for ~400 s of flight time during a single flyby, by measuring drag on the vehicle. By including a charged particle detector, we can also measure the sputtering-induced charged particle flux incident on Europa's surface - either for a single arc across the surface or for a number of predeployment Jovian orbits while onboard the Europa Multiple-Flyby Mission - depending on the length of time the instrument is powered on. In addition to providing highly complementary science to the Europa Multiple-Flyby Mission, the combination of the accelerometer and charged particle detector will yield important insights for the study of Europa's atmosphere and surface composition, its interaction with the Jovian magnetosphere, and possibly links to its subsurface ocean.
This presentation will be focused on the technical challenges of the DARCSIDE mission. The major challenges to be discussed will include how to survive with only one twenty-fifth the energy available at the Earth, this has significant implications for spacecraft temperature and electrical power generation. Additionally, survival in the extreme Jovian radiation environment will be discussed, along how to meet planetary protection requirements for Europa, which requires DARCSIDE to never impact Europa. Finally, the design for the DARCSIDE drag system, and accelerometers will be discussed.
A Europa CubeSat Concept Study for Measuring Europa's Atmosphere
This presentation is the product of a nine-month mission concept study for a CubeSat that would be carried aboard the JPL Europa Multiple-Flyby Mission, released in the Jovian system and make measurements at Europa. We examined the scientific return as well as the technical feasibility of a CubeSat designed to study the linkage between Europa's radiation environment which generates Europa's atmosphere through sputtering and radiolytic processes, and its atmospheric structure. This would be accomplished by measuring a) energetic particles at Europa and b) its atmospheric density through drag forces on the CubeSat. The findings of our concept study for the Deployable Atmospheric Reconnaissance CubeSat with Sputtering Ion Detector at Europa (DARCSIDE) indicate that the technology exists to enable a 3U, 4.4 kg CubeSat to detect Europa's tenuous atmosphere beginning ~200 km above the surface for ~400 s of flight time during a single flyby, by measuring drag on the vehicle. By including a charged particle detector, we can also measure the sputtering-induced charged particle flux incident on Europa's surface - either for a single arc across the surface or for a number of predeployment Jovian orbits while onboard the Europa Multiple-Flyby Mission - depending on the length of time the instrument is powered on. In addition to providing highly complementary science to the Europa Multiple-Flyby Mission, the combination of the accelerometer and charged particle detector will yield important insights for the study of Europa's atmosphere and surface composition, its interaction with the Jovian magnetosphere, and possibly links to its subsurface ocean.
This presentation will be focused on the technical challenges of the DARCSIDE mission. The major challenges to be discussed will include how to survive with only one twenty-fifth the energy available at the Earth, this has significant implications for spacecraft temperature and electrical power generation. Additionally, survival in the extreme Jovian radiation environment will be discussed, along how to meet planetary protection requirements for Europa, which requires DARCSIDE to never impact Europa. Finally, the design for the DARCSIDE drag system, and accelerometers will be discussed.
