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MAMBO PRE-LAUNCH CALIBRATION CONSIDERATIONS
S. Gulkis Paris Meeting February 4-6, 2002
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CALIBRATION OVERVIEW FOUR LEVEL WORK BREAKDOWN
RADIOMETRIC CALIBRATION SPECTRAL CALIBRATION TELESCOPE PARAMETERS BORESIGHT AND MIRROR POSITIONS
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RADIOMETRIC CALIBRATION
Requirement brightness temperature between space and atmosphere known to within 1% (3) or noise level RMS sensitivity less than 1 K in 1 sec Calibration budget considerations Optical system Emissivity and temperature knowledge of calibration target System linearity Gain stability (Alan variance) Sideband ratio (calibration target and mirror alignment covered later) Performance measurements System temperature Bandwidth
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SPECTRAL CALIBRATION Requirement Spectral budget considerations
Frequency knowledge to 1 m/sec - f/f < 1.0/3e8 = 3.3 e (-9) Frequency stability to 3.16 m/sec - f/f < 3.16/3e8 = 1 e (-8) Spectral response of filters /relative gain of spectral channels to 1% Knowledge of sideband ratio to TBD % Spectral budget considerations USO and frequency synthesizers Frequency response of spectrum analysers and filters Including stability Sideband responses /rejection Temperature suceptabilities
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Wind Noise due to Frequency Jitter
Requirement Frequency jitter shall produce an error less than .5 m/sec at 10 m/sec Implication for frequency stability f/f < 3.16/3e8 = 1 e (-8) Derivation |xm -xt| < 0.5 xm = measured wind speed = √(xt2 +x2) xt = true wind speed = 10 m/sec; x = freq. jitter (x/xt)2 = 2 (0.5)/xt x(rms) = 3.16 m/sec at xt = 10 m/sec Corresponds to 100 kHz at 10 Mhz √( )= 10.5
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Telescope Parameters Requirements HPBW TBD
Main beam efficiency >> 0.9 TBD Sidelobe levels >> -30 db TBD
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BORESIGHT AND MIRROR POSITIONS
Requirements Boresight direction shall known to within 0.2 HPBW and aligned with known WRT SC axis to within xxx Boresight stability shall be within 0.05 HPBW Considerations Scan mechanism position, repeatability and jitter S/C Stability
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