Results from the Atomic Oxygen Experiment on the STRV-1a spacecraft
Results from the Atomic Oxygen Experiment on the STRV-1a spacecraft
 
  Anexperiment to makein situ measurements of thermospheric atomicoxygen fluxes andtheir effect on some common spacecraft materials has been flown in orbit on board the SpaceTechnology Research Vehicle 1amicrosatellite. The results from active sensors were based on resistance measurements of silver films and were interpreted relative to space simulationsmade in a ground-based pulsed laser atomic oxygen source. It was concluded that silver
resistance sensors can be used to measure atomic oxygen fluxes but are best suited to low flux environments, e.g., <10(14) atoms cm-2 s-1. Some silver sensors were overlaid with thin coatings to measure the erosion resistance of the coating materials. It was found that erosion rates were affected by the structure of the materials; this structure must therefore be taken into account in experiment and spacecraft design.
  
  647-652
  
    
      Harris, I.L.
      
        06a4182b-467d-4b99-9e4b-794cc91e7ffe
      
     
  
    
      Chambers, A.R.
      
        c6029372-f78a-4f0f-8c80-dfcf1ddf5dbf
      
     
  
    
      Roberts, G.T.
      
        7fb6b314-969b-412d-aed6-0d15fd5624fb
      
     
  
  
   
  
  
    
      1998
    
    
  
  
    
      Harris, I.L.
      
        06a4182b-467d-4b99-9e4b-794cc91e7ffe
      
     
  
    
      Chambers, A.R.
      
        c6029372-f78a-4f0f-8c80-dfcf1ddf5dbf
      
     
  
    
      Roberts, G.T.
      
        7fb6b314-969b-412d-aed6-0d15fd5624fb
      
     
  
       
    
 
  
    
      
  
  
  
  
  
  
    Harris, I.L., Chambers, A.R. and Roberts, G.T.
  
  
  
  
   
    (1998)
  
  
    
    Results from the Atomic Oxygen Experiment on the STRV-1a spacecraft.
  
  
  
  
    Journal of Spacecraft and Rockets, 35 (5), .
  
   
  
  
   
  
  
  
  
  
   
  
    
      
        
          Abstract
          Anexperiment to makein situ measurements of thermospheric atomicoxygen fluxes andtheir effect on some common spacecraft materials has been flown in orbit on board the SpaceTechnology Research Vehicle 1amicrosatellite. The results from active sensors were based on resistance measurements of silver films and were interpreted relative to space simulationsmade in a ground-based pulsed laser atomic oxygen source. It was concluded that silver
resistance sensors can be used to measure atomic oxygen fluxes but are best suited to low flux environments, e.g., <10(14) atoms cm-2 s-1. Some silver sensors were overlaid with thin coatings to measure the erosion resistance of the coating materials. It was found that erosion rates were affected by the structure of the materials; this structure must therefore be taken into account in experiment and spacecraft design.
        
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      Published date: 1998
 
    
  
  
    
  
    
  
    
  
    
  
    
     
    
  
    
  
    
  
    
  
  
        Identifiers
        Local EPrints ID: 21316
        URI: http://eprints.soton.ac.uk/id/eprint/21316
        
        
        
          ISSN: 0022-4650
        
        
          PURE UUID: 8568f7cd-4b6d-48f5-8bd8-f54edf111327
        
  
    
        
          
        
    
        
          
        
    
        
          
        
    
  
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  Date deposited: 23 Nov 2006
  Last modified: 08 Jan 2022 12:51
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      Contributors
      
          
          Author:
          
            
            
              I.L. Harris
            
          
        
      
          
          Author:
          
            
            
              A.R. Chambers
            
          
        
      
          
          Author:
          
            
            
              G.T. Roberts
            
          
        
      
      
      
    
  
   
  
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