Fact Sheet

Text Size

Observation of the Reflective Characteristics of the Spacecraft Plasma Environment from On-Board Thruster Activity Using Ground-Based Instruments (Plasma-Progress)
12.05.12

OpNom:

Overview | Description | Applications | Operations | Results | Publications | Imagery

Experiment Overview

This content was provided by , and is maintained in a database by the ISS Program Science Office.

Brief Summary

Information Pending

Principal Investigator(s)

Information Pending

Co-Investigator(s)/Collaborator(s)

Information Pending

Developer(s)
Information Pending

Sponsoring Space Agency

Russian Federal Space Agency (Roscosmos)

Sponsoring Organization

Information Pending

ISS Expedition Duration:

April 2007 - March 2010



Expeditions Assigned

15,16,17,18,19/20,21/22

Previous ISS Missions

Information Pending

^ back to top



Experiment Description

Research Overview

Information Pending

Description

Determination of space-time relations of the density of the spacecraft plasma environment arising during operation of its onboard liquid-propellant engines

^ back to top



Applications

Space Applications

Information Pending

Earth Applications

Information Pending

^ back to top



Operations

Operational Requirements

Progress TCV nominal propulsion system; Ground facilities of radio observation - incoherent dissipation radar of Solar-Terrestrial Physics Institute, Siberian Center of the Russian Academy of Sciences (Irkuts).

Operational Protocols

Determination of parameters (reflecting characteristics, sizes, density etc.) of large-scale plasma formations arising during operation of Progress TCV vernier thrusters and positioning and attitude control thrusters with different directivity of thruster plumes w.r.t. SC motion direction. Adaptation of the physical model of plasma sheath forming in the SC vicinity as applied to the Progress TCV. Study of interaction of plasma formations around low-orbit SC with ionospheric drag and solar radiation. Analysis of the impact of PS plume exhaust on the radio configuration of a low-orbit SC by comparing the Progress TCV reflecting characteristics when thrusters are operating and not operating.

^ back to top



Results/More Information

Prediction of ISS plasma environment parameters in the periods of nominal operation of engines of different thrust and in case of gas and plasma emissions.

^ back to top



Related Websites
  • Energia - Science Research on the ISS Russian Segment
  • Coordinating Scientific and Technical Council of the Russian Space Agency [Russian]
  • ^ back to top



    Imagery

    Information provided by the investigation team to the ISS Program Scientist's Office.
    If updates are needed to the summary please contact JSC-ISS-Program-Science-Group. For other general questions regarding space station research and technology, please feel free to call our help line at 281-244-6187 or e-mail at JSC-ISS-Payloads-Helpline.