The following article has been published in the
Proceedings of the ESA Symposium "The Far Infrared And Submillimetre Universe" 15-17 April 1997, Grenoble, France, ESA SP-401 (August 1997) pp. 201-206


Stratospheric Observatory for Infrared Astronomy (SOFIA)

 

E. E. Becklin

 

Division of Astronomy and Astrophysics, UCLA, 405 Hilgard Ave., Los Angeles, CA 90095-1562

E-mail: becklin@sofia.astro.ucla.edu; Tel: (310) 206-0208; Fax: (310) 206-2096

 

 

Abstract

The joint US and German SOFIA project to develop and operate a 2.5 meter infrared airborne telescope in a Boeing 747-SP began earlier this year. Universities Space Research Association (USRA), teamed with Raytheon E systems and United Airlines, was selected by NASA to develop and operate SOFIA. The 2.5 meter telescope will be designed and built by a consortium of German companies lead by MAN-GHH. Work on the aircraft and the primary mirror has started. First science flights will begin in 2001, and the observatory is expected to operate for over 20 years. The specifications, instruments and science potential of SOFIA are discussed.

 

Introduction

The Stratospheric Observatory For Infrared Astronomy (SOFIA) is NASA's and DLR's premier observatory for infrared and submillimeter astronomy into the next century. A Boeing 747-SP aircraft will carry a 2.5-meter telescope designed to make sensitive infrared measurements of a wide range of astronomical objects. It will fly at and above 12.5 km, where the telescope collects radiation in the wavelength range from 0.3 micrometers to 1.6 millimeters region of the electromagnetic spectrum.

A team led by the Universities Space Research Association - USRA - has been selected by NASA to design, assemble, test, and operate SOFIA. USRA heads up a team that includes United Airlines, Raytheon E-Systems, Sterling Software, University of California, the SETI Institute, and the Astronomical Society of the Pacific. As part of NASA's privatization program to lower costs and improve efficiency, the SOFIA program has been contracted out to this team. Contract management will be performed by NASA Ames Research Center. The telescope and 20% of operations will be supplied by Germany.

 

Team Members

The prime contractor, USRA, is a 26-year-old consortium of more than 80 universities set up to manage scientific research programs. USRA will have overall project responsibility and will manage the scientific operations of the observatory.

United Airlines, the world's largest air carrier, has provided the Boeing 747-SP to NASA, and will manage SOFIA's flight operations out of the Moffett Federal Airfield near San Francisco, California, traditional home of NASA's airborne astronomy program. Routine maintenance operations will be performed at United's facilities at San Francisco and Oakland.

Raytheon E-Systems of Waco, Texas will do the extensive aircraft modification required to build SOFIA. The five-year job of modifying the airplane for its new scientific role includes installing the telescope and the all-important mission control and communications systems for the observatory. The specialized computer systems needed to operate the telescope will be designed and integrated by Sterling Software.

The USRA/SOFIA Science Center will be located in hangar N211 at NASA Ames Research Center during both development and operation of the observatory. The University of California at Los Angeles and the University of California at Berkeley will be working closely with the USRA/SOFIA team to help provide scientific and technical support for the staff and facility. NASA Ames Research Center will also support the Science Center development through SOFIA work packages. Observatory instruments to be attached to the telescope will be designed and built at US universities and national centers through a peer review process. The German science community will also provide instruments.

 

Germans Supply Telescope and

Utilize 20% of Observing

DLR, Germany's space agency, is funding the design and construction of the telescope in cooperation with NASA. The telescope will be built by MAN GHH, MAN Technologies and Kaiser Threde of the Federal Republic of Germany. During operation, German scientists will utilize 20 percent of the flying observatory's telescope time. DLR will also provide 20 percent of the operations support through on site staffing, telescope maintenance and other provisions.

 

First Light Expected in 2001

SOFIA will see first light in 2001, and is planned to make more than 120 scientific flights of at least 8 hours duration per year. SOFIA is expected to operate for at least 20 years, primarily from Moffett Federal Airfield, but occasionally from other bases around the world, especially in the Southern Hemisphere. SOFIA will fly over 12.5 km, where the typical water vapor column density is less than 5 m m. Typical atmospheric trans-mission at this altitude is shown in Fig. 1, taken from Erickson (1995).

Presently, the SHOTT Zerodur mirror is being ground in Meinz, Germany. A picture of the SOFIA mirror is shown in Fig. 2. The Boeing 747-SP airplane was dedicated in San Francisco in March 1997 and is shown in Fig. 3. The SOFIA telescope will be delivered to Waco, TX in late 2000 for integration.

 

System Characteristics

 

Nominal Operational Wavelength Range: 0.3 to 1600 microns; prime wavelengths 15-300 microns

Primary Mirror Diameter = 2.7 meters

System Clear Aperture Diameter = 2.5 meters

Nominal System f-ratio = 19.6

Primary Mirror f-ratio = 1.28

Telescope's Unvignetted Elevation Range:

20-60 degrees

Optical Configuration: Bent Cassegrain with oscillating secondary mirror and flat folding tertiary.

Unvignetted Field-of-View Diameter = 8 arcmin

Maximum Chop Throw on Sky = ± 5 arcmin

(vignetted); ± 4 arc min (unvignetted)

Chopper Frequencies = 1 to 20 Hz for 2-point square wave chop

Pointing Stability

= 0."2 rms when using on-axis Focal Plane tracking

= 0."8 rms when using on-axis Fine-Field tracking

Pointing Accuracy

= 0."5 when using on-axis Focal Plane tracking

= 3" when using on-axis Fine-Field tracking

Sky Rotation Freeze Mode available for a sky rotation range of +3 degrees (i.e. 6 minutes in time for fast rotators)

Diffraction-Limited Wavelengths > 15 microns

Image Quality of Telescope Optics at 0.6 microns=1.5 arcsec on-axis (80% encircled energy)

 

Chopped Image Quality due to coma for ± 4' Chop Throw

=9."1 for 80% encircled energy diameter

=5."8 for 50% encircled energy diameter

(Chopped Image Quality for other chop throws scale linearly with throw, down to the diffraction-limit or optical quality of the optics.)

Total Emissivity of Telescope (Goal):

15% at 10 microns with dichroic tertiary

10% at 10 microns with aluminized tertiary

Recovery Air Temperature in Cavity (and Optics Temperature)=240K

960 successful flight hours per year between 12.5 km and 14 km in full operations

Will support both state of the art Facility Class and PI Class instruments which can be removed after each flight series

 

Sensitivity

With the parameters given above under the systems characteristics and assuming array detectors, we calculate that the background limited NEFD at 100 m m in a 30% band should be about 400 mJy Hz-1/2 and at 450 m m about 200 mJy Hz-1/2. The corresponding 1s noise in an hour integration should be 7mJy at 100 m m and 3.5 mJy at 450 m m. The 1s line flux limit in 1 hour should be about 3 x 10-18 Wm-2 at a resolution of 103 at 100 m m.

It is instructive to compare the time to make an observation on FIRST and SOFIA. This is done in Table 1 where the observing time on SOFIA is ratioed to a similar observing time on FIRST, for a point source and R<104. The factors considered are the area of the telescopes, the thermal background, the effective emissivity and the transmission. The product of all effects shows that FIRST is 112 times faster than SOFIA. The signal to noise on a point source will be about 11 times greater on FIRST than SOFIA for the same integration time.

For spatial surveys, the situation will probably be different, since SOFIA can use an advanced large format array at some future date. For example, at 100 m m the proposed FIRST array is 25x16 pixels. The SOFIA 8 arcmin field can effectively use a Nyquist sampled array with 128x128 pixels. This implies a factor of 32 decrease in time for spatial surveys or maps with SOFIA. Thus for 100 m m survey observations FIRST will have about twice the signal to noise of SOFIA for the same observation time.

 

Instrumentation

From the US side, SOFIA instruments will be selected for development by peer review of submitted proposals. In the USRA call for proposals, both Facility Class and PI class instruments were requested. It is anticipated that one or two Facility Class instruments will be delivered to the USRA Science Center during the first year of operation. The Facility Instruments are expected to be user friendly and will not require the builder to be present to operate. One member of the Science Center will work with the team developing a Facility Instrument (FI) and FIs will have PDRs and CDRs conducted. To cover all the science areas of SOFIA, a number of PI instruments will also be selected for development.

Table 2 shows the US SOFIA instruments selected by NASA for feasibility studies in 1996. It is anticipated that fewer than half of these instruments will be developed in the first call. The Germans are expected to develop P.I. class instruments. A list of possible German instruments is given in Table 3.

 

Science Potential

The primary wavelength regions where SOFIA will work are important for the following astrophysical reasons:

  1. Most of the fundamental absorption and emission lines and bands of astrophysically and astrochemically significant molecules occur in this region;

  2. Most of the luminosity of our galaxy and in other galaxies emerges in this wavelength region;

  3. Low dust extinction at these wavelengths permits unbiased and potentially complete observations of statistically large samples of objects; and

  4. Formation of galaxies in the early universe and the crucial stages of formation of stars and planets can be best studied in this range of wavelengths.

Complementing present and future infrared astronomical experiments, SOFIA will image to the "confusion limit" of the extremely sensitive Space InfraRed Telescope Facility (SIRTF) at 150 m m in about one hour but with a beam area that is 10 times smaller. SOFIA will provide a sensitive platform for both imaging and spectroscopy at wavelengths longer than the 200 m m limit of the Infrared Space Observatory and SIRTF. SOFIA complements the newly commissioned Keck Telescopes in Hawaii and other large ground-based telescopes scheduled for operation in the next decade to perform imaging and spectroscopy in the near infrared atmospheric windows from 1 to 30 m m. SOFIA provides imaging beyond 30 m m, allows spectroscopy in the regions between atmospheric windows and unique high resolution spectroscopy of absorption and emission lines of molecules, including biogenic material, from 30 to 300 m m. SOFIA's spatial resolution in the far-infrared will match those of the submillimeter 10-meter class ground-based telescopes such as the Caltech Submillimeter Observatory and the James Clark Maxwell Telescope in Hawaii.

 

Acknowledgements

I would like to thank Jackie Davidson, Jim Kolonko, James Musser and many others on the USRA SOFIA Team for help with putting this paper together.

 

References

Erickson, E. F. 1995, SOFIA: The Next Generation Airborne Observatory, Space Sci. Reviews, 74, 91-100.

 

Table 1. Observation Time of SOFIA vs FIRST

 

SOFIA

FIRST

f(t)

t(ratio)

Area Telescope

2.5m

3.25m

D4

2.9

Background (temperature)

240K

80K

Bn (T)

6

Emissivity

.25

.06

Î

4.1

Trans. (1-Î )

.75

.94

(1-Î )2

1.6

 

Table 2. FY96 SOFIA Instrument Technology Studies Funded by NASA

Principa
Investigator

Institution Instrument

Betz, A.

U. CO, Boulder

A Far-Infrared Heterodyne Spectrometer

Bregman, J.

NASA-ARC

Study of a Mid-Infrared Spectral Imager

Clemens, D.

Boston U.

IMPP: A Far-Infrared Imaging Photometer and Polarimeter design study

Elliot, J.

Lowell Obs.

Airborne Occultation Studies of the Solar System

Erickson, E. & Haas, M.

NASA-ARC

Technology Development for an Airborne Infrared Echelle Spectrometer (AIRES)

Garden, R.

U. C. Irvine

MIR2CAM: A Two-Channel Mid-Infrared Camera for Broad-Band Imaging

Greenhouse, M.

NASA-GSFC

A Concept Study for Near-Infrared Spectroscopic Imaging

Harper, D.

Yerkes Obs.

A Far-Infrared Imager

Harvey, P.

U. T., Austin

A Diffraction-Limited, Multi-Color Far-Infrared Camera

Herter, T.

Cornell U.

FOCUS: A Faint-Object Spectrograph

Hildebrand, R.

U. Chicago

A Polarimeter for SOFIA

Lacy, J.

U. T., Austin

A Very High Resolution Mid-Infrared Spectrograph

Moseley, S.

NASA-GSFC

Study and Preliminary Design of the Submillimeter and Far-Infrared Experiment (SAFIRE)

Stacey, G.

Cornell U.

SWIFT: A Widefield Imaging Fabry-Perot

Walker, C.

Steward Obs.

A 2 Thz Heterdyne Array Receiver

Young, E.

Steward Obs.

A Far-Infrared Camera for SOFIA

Zmuidzinas, J.

Cal-Tech

Airborne Submillimeter Spectroscopy

 

Table 3.

Liste der geplanten deutschen SOFIA Beobachtungsinstrumente

Stand 21. November 1996

Principal
Investigator
Institut nstrument Partner Welien-
Längen Bereich
Spektrale
Auflösung
A. Poglitsch MPE, Garching

Abbildendes Spektro/Photometer

Universität Jena

40-350 m m

5 - 5 .104
E. Kreysa

MPlfR, Bonn

Bolometer Instrument

>300 m m

G. Arnold

DLR Planetener-kundung, Berlin

Abbildendes Spektrometer

0.8-5 m m
R. Schieder Universität Kö1n IR-Heterodyn-System

5-16 m m

3 › 107
G. Schwaab DLR Weltraum-sensorik, Berlin Heterodyn-System MPlfR, Bonn
DLR-OE, Oberpfaffenhofen
Universität Köln
>2-6 THz <106
J. Stutzki Universität Kö1n Heterodyn-Array MPlfR, Bonn
IRAM, Grenoble >
1-2 THz 106
J. Wolf DLR Weltraum-sensorik, Berlin <

Spektral-Photometrische Kamera

UoC/LBL, Berkeley, MPIA, Heidelberg, UoF, Gainesville

NASA/ARC

20 - 240 m m

2 - 5
50 - 100

 

graph showing atmospheric transmissin versus wavelength

photo of telescope blank

Fig. 2. The SOFIA primary mirror blank. It is being cut from a blank of Zerodur™ by Schott Glaswerke in Mainz, Germany (near Frankfurt), under contract with Kayser-Threde and MAN-GHH. The blank was over 3 meters and has been cut to 2.7 meters for use on SOFIA. Final mirror weight after lightweighting will be about 850 kilograms (1,900 pounds). The Zerodur material is a unique glass ceramic material developed by Schott that effectively has zero thermal expansion characteristics. Final polishing will be performed at REOSC in Paris, France.

 

 

Dr. Charles H. Townes giving speech at didication ceremony

Fig. 3. Dr. Charles H. Townes, Nobel prize-winning physicist and KAO user at the University of California, Berkeley, gave one of the keynote speeches at the aircraft dedication ceremony. The SOFIA aircraft, originally dedicated in 1977 as the "Clipper Lindbergh", is in the background.