Venus Probe (DAVINCI) Gas Ingestion System

Venus Probe (DAVINCI) Gas Ingestion SystemVenus Probe (DAVINCI) Gas Ingestion SystemVenus Probe (DAVINCI) Gas Ingestion SystemVenus Probe (DAVINCI) Gas Ingestion System
  • Home
  • Venus Exploration History
  • Gas Ingestion System
  • Our Work with NASA JPL
  • Experimental Model
  • Mathematical Model
  • Updates
  • Meet the Team

Venus Probe (DAVINCI) Gas Ingestion System

Venus Probe (DAVINCI) Gas Ingestion SystemVenus Probe (DAVINCI) Gas Ingestion SystemVenus Probe (DAVINCI) Gas Ingestion System
  • Home
  • Venus Exploration History
  • Gas Ingestion System
  • Our Work with NASA JPL
  • Experimental Model
  • Mathematical Model
  • Updates
  • Meet the Team

DAVINCI Probe

As it descends through the atmosphere, the DAVINCI probe will collect gas samples from the atmosphere at different altitudes. A gas inlet located on the probe's exterior will suck up the gases and, through a series of pipes and valves, make its way to the VTLS for data transmission back to Earth.

VTLS

The Venus Tunable Laser Spectrometer (VTLS) is a device within the DAVINCI probe. The VTLS will study the chemical reactions in the upper atmospher and the near-surface environment. Additionally, the VTLS will detect key gas species containing Hydrogen, Sulfur, Carbon and Oxygen, as well as high precision measurements of the Deuterium to Hydrogen ratios at various altitudes.

Our Mission

The goal will be to validate a nominal subsystem design, including restrictor and tubing geometries as well as valve timing, and produce a probabilistic assessment of the subsystem dynamics given uncertainties in inlet conditions and component characteristics. This analysis will inform the development of requirements and tolerances, including future plans for hardware verification and validation. The final deliverable for the project will be a report detailing the analyses performed and the simulation and modeling results, with a particular focus on design recommendations, uncertainties, and any perceived model limitations based on an understanding of the mission environments.

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Stevens Institute of Technology

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