return to hubble: servicing mission 4 dr. frank summers space telescope science institute april 2,...
TRANSCRIPT
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Return to Hubble: Servicing Mission 4
Dr. Frank SummersSpace Telescope Science Institute
April 2, 2009
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A Space Telescope
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Artist’s Illustration
WRONG
Photograph
CORRECT
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Size of Earth
Size of Earth’s Atmosphere
6400 km
600 km above surface
Size of Hubble’s Orbit
100 km above surface
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Some Hubble History
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• 1946 – Space telescope proposed
• 1962 – National Academy of Sciences recommends
Lyman Spitzer
• 1976 – NASA & ESA collaborate• 1977 – Congress funds project• 1985 – Construction complete• 1986 – Challenger accident
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• 1990 – Launch• 1993 – Servicing Mission 1• 1997 – Servicing Mission 2• 1997 – Mission extended
from 15 to 20 years• 1999 – Servicing Mission 3A• 2002 – Servicing Mission 3B• 2003 – Columbia accident• 2004 – No shuttle mission?• 2005 – Two gyro mode• 2006 – “One final house
call”• 2008 – Hardware delay
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What Makes Hubble So Great?
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• Clear View – located above blurring effects of atmosphere
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• Serviceable – new instruments every few years keeps it current
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• Public – Observers get only one year of exclusive access
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• Professional – STScI provides excellent support to scientists
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Houston, We Have a Problem
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Hubble Servicing Missions
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Servicing Mission 1 – December 1993
• COSTAR, WFPC2
• solar arrays, gyros
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Servicing Mission 2 – February 1997
• NICMOS, STIS
• fine guidance sensor, solid state recorder, reaction wheel assembly
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Servicing Mission 3A – December 1999
• gyroscope failure in November
• computer, data recorder, fine guidance sensor, electronics improvement, thermal protection
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Servicing Mission 3B – March 2002
• ACS
• solar arrays, NICMOS cooling system, reaction wheel assembly, power control unit
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Servicing Mission 4 – May 2009
• WFC3, COS
• ACS repair, STIS repair, gyros, batteries, fine guidance sensor, thermal blanket, de-orbit module
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Servicing Mission 4 – May 2009
• WFC3, COS
• ACS repair, STIS repair, gyros, batteries, fine guidance sensor, thermal blanket, de-orbit module
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1990
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1993
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1997
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2002
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2009
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Hubble, We Have an Anomaly
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SM4: An Ambitious Workload
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SM4: An Ambitious Workload
“This final mission will be, without doubt, the most complicated and challenging that NASA has ever mounted.”
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Major Goals for SM4
1 Enhance Hubble’s scientific capabilities with a new camera and new spectrograph• WFC3, a panchromatic camera, replacing WFPC2
• COS, a very efficient spectrograph, replacing COSTAR
2 Restore existing Hubble capability through in-situ repair• STIS: repair failed electronics
• ACS: repair failed electronics
3 Upgrade Hubble to last to beyond 2014• Install refurbished Fine Guidance Sensor
• Install 6 new gyros
• Install 6 new batteries
• Install thermal protection covers
• Install Capture Mechanism for de-orbit mission
If successful, HST will be at the height of its power,
with 6 working, complementary, science instruments
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NOTE: Now that SM4 is officially manifested and a crew has been assigned, the EVA timeline is controlled by the Space Shuttle Program.
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Wide Field Camera 3
– WFC3…
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Wide Field Camera 3
• WFC3 has two wide field cameras– near ultraviolet and optical imaging
(UVIS)– near infrared imaging camera (IR)
• First truly panchromatic camera• Improves on ACS & NICMOS
– UVIS >30x discovery power of ACS/WFPC2– IR 15-20x discovery power of NICMOS
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Camera Comparison
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Cosmic Origins Spectrograph
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Cosmic Origins Spectrograph
• COS optimized for ultraviolet observations• Far Ultraviolet Channel
– 1-reflection, aberration-corrected along dispersion– 2 side-by-side 16k by 1k pixel detector (FUSE design)– Records arrival time of every detected photon– 3 gratings; 300 or 800 (nm) spectral range– Resolving power ~3000, ~20,000 [115 to 205 nm]
• Near Ultraviolet Channel– Fully corrected optical design– 1k by 1k pixel detector (STIS design)– Records arrival time of every detected photon– 4 gratings– 10 to 80 nanometers spectral ranges– Resolving power ~2000, ~20,000 [170 to 320 nm]
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COS vs STIS
Limiting Flux for S/N=10 in 3600 sec (R~10,000 (0.15 Ǻ) binning)
-15.5
-15.0
-14.5
-14.0
-13.5
-13.0
-12.5
1100 1200 1300 1400 1500 1600 1700 1800
Wavelength (Ǻ)
log
Flu
x (
erg
cm
-2 s
ec-1
Ǻ-1)
STIS E140MR=45,000
STIS G140MR~11,000-17,000
COS G130MR~20,000-24,000
COS G160MR~20,000-24,000
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ACS Repair
• Advanced Camera for Surveys• ACS failure in January 2007• Cut through a grill• Similar to WFC3, but …
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STIS Repair
• Space Telescope Imaging Spectrograph
• STIS failure in August 2002• > 100 fasteners• Similar to COS, but …
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Gyros
• 3 gyros operating is nominal• 2 gyro mode since 2005• 3 failed, 2 operating, 1 spare
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Gyros installed in SM3A
0
1
2
3
4
5
6
7
8
G1 G2 G3 G4 G5 G6
RR
RR
Solid blue = run tim e @ SM3BSlant blue = run tim e @ 9/17/07Red = run tim e @ pre-SM3B failureSlant red = run tim e @ pos t-SM3B failureRR = rotor res triction failure
Gyros in HST at completion of SM1
0
1
2
3
4
5
6
7
8
G1 G2 G3 G4 G5 G6
Ru
n-t
ime
in
Ye
ars
FL
FL
FL
FL
Solid blue = run tim e @ SM2Slant blue = run tim e @ SM3ARed = run tim e @ failureFL = flex lead failure
50% failure probability
75% failure probability
95% failure probability
ON
OFF
FL
ON
G1 G2 G3 G4 G5 G6 G1 G2 G3 G4 G5 G6
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Batteries
• Hubble can not point without batteries
• About 100,000 charge-discharge cycles
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Bay 8 Thermal Situation
BAY9
BAY8
SM3B Survey
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Bay 8 Thermal Situation•Patched during SM2, however expected to
be completely degraded
PATCHBAY 7 BAY 8
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Bay 8 Thermal Situation
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• Possible severe scheduling impacts
Possible Bay 8 Impacts
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SM4 Preparations
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HFMS Fit Check
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HFMS Fit Check
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ASIPE Fit Check
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HST equipment at KSC
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May 12, 2009
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