20240017852. SATELLITE CONFIGURATION FOR OPERATION IN THE THERMOSPHERE simplified abstract (Earth Observant Inc.)

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SATELLITE CONFIGURATION FOR OPERATION IN THE THERMOSPHERE

Organization Name

Earth Observant Inc.

Inventor(s)

Christopher Thein of El Granada CA (US)

Nathan Rosenblad of El Granada CA (US)

James Dicorcia of El Granada CA (US)

SATELLITE CONFIGURATION FOR OPERATION IN THE THERMOSPHERE - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240017852 titled 'SATELLITE CONFIGURATION FOR OPERATION IN THE THERMOSPHERE

Simplified Explanation

The patent application describes a satellite designed to operate in the thermosphere and powered by an electric rocket engine. The satellite includes a remote sensing system that captures images of the Earth. The satellite has a longitudinally elongated body with an elongated axis aligned with the forward direction of the satellite. The center of mass is positioned forward of the center of drag to ensure positive natural stability. The remote sensing system includes movable mirrors and optical elements that can be pivoted or rotated around the axis of the elongated body. Counter-acting masses are used to nullify the motion of the movable components.

  • The satellite is capable of operating in the thermosphere.
  • It is powered by an electric rocket engine.
  • The satellite includes a remote sensing system to capture images of the Earth.
  • The elongated body of the satellite is aligned with the forward direction.
  • The center of mass is positioned forward of the center of drag for stability.
  • The remote sensing system includes movable mirrors and optical elements.
  • Counter-acting masses are used to prevent motion of the movable components.

Potential Applications:

  • Earth observation and imaging
  • Climate monitoring
  • Disaster management and response
  • Environmental research and analysis
  • Military surveillance

Problems Solved:

  • Operating in the thermosphere, which is a challenging environment for satellites.
  • Achieving positive natural stability for the satellite.
  • Capturing high-quality images of the Earth from space.
  • Allowing flexibility in adjusting the viewing angle and orientation of the remote sensing system.

Benefits:

  • Improved satellite stability and maneuverability.
  • Enhanced image quality and resolution.
  • Increased flexibility in capturing images from different angles.
  • Potential for a wide range of applications in various industries.


Original Abstract Submitted

a satellite having a longitudinally elongated body and being capable of operating in the thermosphere. the satellite can be powered by an electric rocket engine, and includes a remote sensing system configured to obtain images of earth. an elongated axis about which the elongated body extends can be generally aligned with a forward direction of the satellite, with a viewing angle from the satellite oriented transverse to the elongated axis. a center of mass of the satellite can be forward of a center of drag to produce positive natural stability. the remote sensing system, which can be part of a payload, can include a movable mirror and one or more movable optical elements. a first mirror can be pivoted, and/or other optical elements, including the payload, can be rotated about the axis of the elongated body. counter-acting masses can be used to null motion of the movable components.

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