PDS_VERSION_ID                        = PDS3                                  
RECORD_TYPE                           = FIXED_LENGTH                          
RECORD_BYTES                          = 80                                    
FILE_RECORDS                          = 51                                    
DATA_SET_ID                           = "MGN-V-RSS-1-BSR-V1.0"                
PRODUCT_ID                            = "94156157.QPC"                        
FILE_NAME                             = "94156157.QPC"                        
SPACECRAFT_NAME                       = MAGELLAN                              
INSTRUMENT_ID                         = RSS                                   
TARGET_NAME                           = "VENUS"                               
PRODUCT_VERSION_ID                    = 1                                     
PRODUCT_CREATION_TIME                 = 1994-06-01T21:24:18                   
MISSION_PHASE_NAME                    = "MAPPING CYCLE 6"                     
ORBIT_NUMBER                          = {13034,13035,13036,13037,13038,13039} 
START_TIME                            = 1994-06-05T12:00:00                   
STOP_TIME                             = 1994-06-06T01:00:00                   
SPACECRAFT_CLOCK_START_COUNT          = "N/A"                                 
SPACECRAFT_CLOCK_STOP_COUNT           = "N/A"                                 
^DESCRIPTION                          = "QTERNION.TXT"                        
NOTE                                  = "The calculated values of the         
    attitude quaternions, just prior to the first experiment and just         
    after the last experiment are:                                            
                                                                              
        Date/Time (SCET)      Q1         Q2         Q3         Q4             
      ------------------- ---------- ---------- ---------- ----------         
      94-156/13:02:05.800  0.6664385 -0.5093185  0.4605714  0.2903927         
      94-157/00:15:35.131  0.6678308 -0.5069345  0.4630998  0.2873286         
                                                                              
    The polynomial reference times (TTF, in SCET) and the start and stop      
    execution times for each orbit are:                                       
                                                                              
            Orbit 13034:                                                      
             94-156/16:08:00.466  Start Quasi Polynomial Pointing             
             94-156/16:19:25.066  Polynomial Reference Time                   
             94-156/16:30:48.466  End Quasi Polynomial Pointing               
                           Attitude Knowledge Error= 0.097 degrees            
                                                                              
            Orbit 13035:                                                      
             94-156/17:40:57.799  Start Quasi Polynomial Pointing             
             94-156/17:52:22.533  Polynomial Reference Time                   
             94-156/18:03:45.799  End Quasi Polynomial Pointing               
                           Attitude Knowledge Error= 0.102 degrees            
                                                                              
            Orbit 13036:                                                      
             94-156/19:13:55.132  Start Quasi Polynomial Pointing             
             94-156/19:25:20.000  Polynomial Reference Time                   
             94-156/19:36:43.132  End Quasi Polynomial Pointing               
                           Attitude Knowledge Error= 0.098 degrees            
                                                                              
            Orbit 13037:                                                      
             94-156/20:46:52.465  Start Quasi Polynomial Pointing             
             94-156/20:58:17.466  Polynomial Reference Time                   
             94-156/21:09:40.465  End Quasi Polynomial Pointing               
                           Attitude Knowledge Error= 0.100 degrees            
                                                                              
            Orbit 13038:                                                      
             94-156/22:19:49.798  Start Quasi Polynomial Pointing             
             94-156/22:31:14.933  Polynomial Reference Time                   
             94-156/22:42:37.798  End Quasi Polynomial Pointing               
                           Attitude Knowledge Error= 0.099 degrees            
                                                                              
            Orbit 13039:                                                      
             94-156/23:52:47.131  Start Quasi Polynomial Pointing             
             94-157/00:04:12.400  Polynomial Reference Time                   
             94-157/00:15:35.131  End Quasi Polynomial Pointing               
                           Attitude Knowledge Error= 0.102 degrees  "         
END