160µm Focal Plane Survey, Coarse

Principal: Jocelyn Keene
Deputy: Jane Morrison, Bill Wheaton
Data Monkey(s): Jane Morrison and Bill Wheaton
Priority: Critical
Downlink Priority: Normal
Analysis Time: Campaign J: 3600 minutes, Campaign K: 3600 minutes. Combining both J and K 120 minutes.
Last Updated:


Objective

To measure the location of the 160 µm array relative to the PCRS.

Description

Put the CSMM in a position to direct light from a bright 160 µm source onto the 160 µm array. Step the image across the array by moving the spacecraft in 16 arc second steps for a total 6 steps. At each step using the CSSM to chop off the source. Integrate 3 sec each on and off the source along the slit. Insert each scan above within the standard FPS "PCRS sandwich" measurements and a set of stim observations. Dither the spacecraft by 8 arcseconds in the v direction and repeat the above observations. Dither the spacecraft by 24 arcseconds in the w direction and repeat the above observations. Dither the spacecraft by 8 arcseconds in the v direction and repeat the above observations. Repeat the above series of observations at 2 other locations along the array.
This task is run in campaigns J and K. The data from each campaign is processed separately by the MIPS and IPF teams. The IPF team then combines the results from both campaigns. The results from the IPF multi-run are used to update Frame Table 12. The frame table updates for all the campaigns can be found in the following table:
Frame Table Updates.

Data Collected

The observing strategy is described below but it is similar to the SED FPS. A total of 360 observations are obtained.

Calibration Star

For the selected calibration star see the IER for this survey. The requirements on the SED focal plane calibration star are as follows:

  • In CVZ
  • Mips requirements: stellar brightness corresponding to S/N of 30 (3 sec integrations) 0.212 Jy, K mag -0.54

    Observing Strategy

    Definitions:

  • W axis direction is defined by the Frame Table, and is always within +/- 90 degrees of the TPF z axis as projected on the sky. Motion along this axis corresponds to motion in the spacecraft motion (left/right).
  • V axis direction is defined by the Frame Table, and is always within +/- 90 degrees of the TPF y axis as projected on the sky. Motion along this axis corresponds to motion in the scan mirror direction (up/down).
  • W offset, the amount of motion in the W direction which results in moving the target along the array for images on the left, middle and right of array.
  • V offset, the amount of motion in the V direction which results in moving the target along the v axis.

    160 µm FPS observational parameters:

  • W offset = 100 arc seconds
  • V offset = 16 arc seconds
  • W dither = 24 arc seconds
  • V dither = 8 arc seconds
  • mirror locations for chopping .
    1. position 1 = 0
    2. position 2 = -75

    Observational Strategy

    Starting at an initial position on the left-side of the array take 120 observation. Move to the center of the array and take another 120 observations. Then move to the right-side of the array and take 120 observations.
  • Step 1 : PCRS observation
  • Step 2. Observations on Left side of array: Position the telescope at initial V and W offset positions, in the arrangement the target will fall on the left side of the array.
  • Step 3 (30 observations)
    1. Dither in the V direction ( 8 arc seconds)
    2. Repeat steps A-E
  • Step 4 (30 observations)
    1. Dither in the W direction ( 24 arc seconds)
    2. Repeat steps A- E
  • Step 5 (30 observations)
    1. Dither in the V direction ( 8 arc seconds)
    2. Repeat steps A- E
  • Step 6: PCRS observation
  • Step 7 (120 observations near the center of the array)
    1. Move the spacecraft in the W direction by W offset (100 arc seconds)
    2. repeat steps 2-5 (except Woffset will put target at the center of the array)
  • Step 8 (120 observations on right-side of array)
    1. Move the spacecraft in the W direction by W offset (100 arc seconds)
    2. repeat steps 2-5 (except Woffset will put target at right-side of array)

    Number of observations from step 2, 30. Step 2 repeated 12 times for a total 360 DCE observations. Number of PCRS observations 4.

    
    

    Data Reformatting Requirements

    Array Data Desired:

    160 µm

    Data Reformatting Option:


    Task Dependencies

    The pointing and tracking must be performing optimally .
    This task should be performed at least 6 hours after the turn on of MIPS

    Calibration Dependencies


    Output and Deliverable Products


    Data Analysis


    Software Requirements


    Actions Following Analysis

    1. After each run 234-J and 234-K the MIPS team recieves the results from the IPF team and reviews them.
    2. The MIPS team reviews the MF file from the multi-run tool and approves or disapproves.
    3. When approved, SSC generates mini-spreadsheet for review and approval by MCCB, followed by handoff to JPL OET, and uplink of FTU #12.

    Failure Modes and Responses


    Additional Notes