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REVIEW ARTICLE the NASA Spitzer Space Telescope
REVIEW OF SCIENTIFIC INSTRUMENTS 78, 011302 ͑2007͒ REVIEW ARTICLE The NASA Spitzer Space Telescope ͒ R. D. Gehrza Department of Astronomy, School of Physics and Astronomy, 116 Church Street, S.E., University of Minnesota, Minneapolis, Minnesota 55455 ͒ T. L. Roelligb NASA Ames Research Center, MS 245-6, Moffett Field, California 94035-1000 ͒ M. W. Wernerc Jet Propulsion Laboratory, California Institute of Technology, MS 264-767, 4800 Oak Grove Drive, Pasadena, California 91109 ͒ G. G. Faziod Harvard-Smithsonian Center for Astrophysics, 60 Garden Street, Cambridge, Massachusetts 02138 ͒ J. R. Houcke Astronomy Department, Cornell University, Ithaca, New York 14853-6801 ͒ F. J. Lowf Steward Observatory, University of Arizona, 933 North Cherry Avenue, Tucson, Arizona 85721 ͒ G. H. Riekeg Steward Observatory, University of Arizona, 933 North Cherry Avenue, Tucson, Arizona 85721 ͒ ͒ B. T. Soiferh and D. A. Levinei Spitzer Science Center, MC 220-6, California Institute of Technology, 1200 East California Boulevard, Pasadena, California 91125 ͒ E. A. Romanaj Jet Propulsion Laboratory, California Institute of Technology, MS 264-767, 4800 Oak Grove Drive, Pasadena, California 91109 ͑Received 2 June 2006; accepted 17 September 2006; published online 30 January 2007͒ The National Aeronautics and Space Administration’s Spitzer Space Telescope ͑formerly the Space Infrared Telescope Facility͒ is the fourth and final facility in the Great Observatories Program, joining Hubble Space Telescope ͑1990͒, the Compton Gamma-Ray Observatory ͑1991–2000͒, and the Chandra X-Ray Observatory ͑1999͒. Spitzer, with a sensitivity that is almost three orders of magnitude greater than that of any previous ground-based and space-based infrared observatory, is expected to revolutionize our understanding of the creation of the universe, the formation and evolution of primitive galaxies, the origin of stars and planets, and the chemical evolution of the universe. -
Wide-Field Infrared Survey Explorer Launch Press
PRess KIT/DECEMBER 2009 Wide-field Infrared Survey Explorer Launch Contents Media Services Information ................................................................................................................. 3 Quick Facts ............................................................................................................................................. 4 Mission Overview .................................................................................................................................. 5 Why Infrared? ....................................................................................................................................... 10 Science Goals and Objectives ......................................................................................................... 12 Spacecraft ............................................................................................................................................. 16 Science Instrument ............................................................................................................................. 19 Infrared Missions: Past and Present ............................................................................................... 23 NASA’s Explorer Program ................................................................................................................. 25 Program/Project Management .......................................................................................................... 27 Media Contacts J.D. Harrington -
ASTR 2310: Chapter 6
ASTR 2310: Chapter 6 Astronomical Detection of Light The Telescope as a Camera Refraction and Reflection Telescopes Quality of Images Astronomical Instruments and Detectors Observations and Photon Counting Other Wavelengths Modern Telescopes Refracting / Reflecting Telescopes 0 Refracting Telescope: Lens focuses light onto the focal plane Focal length Reflecting Telescope: Concave Mirror focuses light onto the focal Focal length plane Almost all modern telescopes are reflecting telescopes. Secondary Optics 0 In reflecting telescopes: Secondary mirror, to re- direct light path towards back or side of incoming light path. Eyepiece: To view and enlarge the small image produced in the focal plane of the primary optics. Disadvantages of 0 Refracting Telescopes • Chromatic aberration: Different wavelengths are focused at different focal lengths (prism effect). Can be corrected, but not eliminated by second lens out of different material. • Difficult and expensive to produce: All surfaces must be perfectly shaped; glass must be flawless; lens can only be supported at the edges. The Best Location for a Telescope0 Far away from civilization – to avoid light pollution The Best Location for a Telescope (II)0 Paranal Observatory (ESO), Chile http://en.wikipedia.org/wiki/Paranal_Observatory On high mountain-tops – to avoid atmospheric turbulence ( seeing) and other weather effects The Powers of a Telescope: 0 Size does matter! 1. Light-gathering power: Depends on the surface area A of the primary lens / D mirror, proportional to diameter squared: A = pi (D/2)2 The Powers of a Telescope (II) 0 2. Resolving power: Wave nature of light => The telescope aperture produces fringe rings that set a limit to the resolution of the telescope. -
Silicon Wafer Integration of Ion Electrospray Thrusters Noah Wittel
Silicon Wafer Integration of Ion Electrospray Thrusters by Noah Wittel Siegel B.S., United States Military Academy (2018) Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY May 2020 © Massachusetts Institute of Technology 2020. All rights reserved. Author.............................................................. Department of Aeronautics and Astronautics May 19, 2020 Certified by. Paulo C. Lozano M. Alemán-Velasco Professor of Aeronautics and Astronautics Thesis Supervisor Accepted by . Sertac Karaman Associate Professor of Aeronautics and Astronautics Chair, Graduate Program Committee 2 Silicon Wafer Integration of Ion Electrospray Thrusters by Noah Wittel Siegel Submitted to the Department of Aeronautics and Astronautics on May 19, 2020, in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics Abstract Combining efficiency, simplicity, compactness, and high specific impulse, electrospray thrusters provide a unique solution to the problem of active control in the burgeoning field of miniature satellites. With the potential of distributed systems and low cost functionality currently being realized through development of increasingly smaller spacecraft, thruster research must adjust accordingly. The logical limit of this rapidly accelerating trend is a fully integrated silicon wafer satellite. Such a large surface area to volume ratio, however, both necessitates propulsion capability and renders other mechanisms of control unfeasible due to their respective form factors. While development of electrospray thrusters has exploded in the past two decades, current architectures are similarly incompatible with a silicon wafer substrate. This thesis examines the design and testing of a novel hybrid electrospray archi- tecture which combines previous successes of both capillary and externally-wetted ge- ometries. -
UV and Infrared Astronomy
Why Put a Telescope In Space? • Access to light that does not penetrate the atmosphere • No seeing. A telescope can reach the diffraction limit: 1.22 l/D radians Astronomy in Space. I. UV Astronomy Ultraviolet Astronomy 912-3650 Å (Lyman Limit to Balmer jump) • Continuua of hot stars (spectral types O,B,A) • H I Lyman lines (1-n transitions) • Resonance lines of Li-like ions C IV, N V, O VI • H2 Lyman and Werner bands Normal incidence optics • Special UV-reflective coatings The Far Ultraviolet 912 to 1150 Å • Defined by Lyman limit, MgF cutoff at 1150 Å • LiF + Al reflects longward of 1050 Å • SiC reflects at shorter wavelengths The Astronomy Quarterly, Vol. 7, pp. 131-142, 1990 0364-9229f90 $3.00+.00 Printed in the USA. All rights reserved. Copyright (c) 1990 Pergamon Press plc ASTRONOMICAL ADVANTAGES History OFAN • 9/1/1946: Lyman Spitzer EXTRA-TERRESTRIAL OBSERVATORY proposed a Space Telescope in LYMAN SPITZER, Jr. ’ a Report to project Rand This study points out, in a very preliminary way, the results that might be expected from astronomical measurements made with a satellite • 1966: Spitzer (Princeton) vehicle. The discussion is divided into three parts, corresponding to three different assumptions concerning the amount of instrumentation provided. chairs NASA Ad Hoc In the first section it is assumed that no telescope is provided; in the second a 10-&h reflector is assumed; in the third section some of the results Committee on the "Scientific obtainable with a large reflecting telescope, many feet in diameter, and revolving about the earth above the terrestrial atmosphere, are briefly Uses of the Large Space sketched. -
The Spitzer Space Telescope and the IR Astronomy Imaging Chain
Spitzer Space Telescope (A.K.A. The Space Infrared Telescope Facility) The Infrared Imaging Chain Fundamentals of Astronomical Imaging – Spitzer Space Telescope – 8 May 2006 1/38 The infrared imaging chain Generally similar to the optical imaging chain... 1) Source (different from optical astronomy sources) 2) Object (usually the same as the source in astronomy) 3) Collector (Spitzer Space Telescope) 4) Sensor (IR detector) 5) Processing 6) Display 7) Analysis 8) Storage ... but steps 3) and 4) are a bit more difficult! Fundamentals of Astronomical Imaging – Spitzer Space Telescope – 8 May 2006 2/38 The infrared imaging chain Longer wavelength – need a bigger telescope to get the same resolution or put up with lower resolution Fundamentals of Astronomical Imaging – Spitzer Space Telescope – 8 May 2006 3/38 Emission of IR radiation Warm objects emit lots of thermal infrared as well as reflecting it Including telescopes, people, and the Earth – so collection of IR radiation with a telescope is more complicated than an optical telescope Optical image of Spitzer Space Telescope launch: brighter regions are those which reflect more light IR image of Spitzer launch: brighter regions are those which emit more heat Infrared wavelength depends on temperature of object Fundamentals of Astronomical Imaging – Spitzer Space Telescope – 8 May 2006 4/38 Atmospheric absorption The atmosphere blocks most infrared radiation Need a telescope in space to view the IR properly Fundamentals of Astronomical Imaging – Spitzer Space Telescope – 8 May 2006 5/38 -
The Evolving Launch Vehicle Market Supply and the Effect on Future NASA Missions
Presented at the 2007 ISPA/SCEA Joint Annual International Conference and Workshop - www.iceaaonline.com The Evolving Launch Vehicle Market Supply and the Effect on Future NASA Missions Presented at the 2007 ISPA/SCEA Joint International Conference & Workshop June 12-15, New Orleans, LA Bob Bitten, Debra Emmons, Claude Freaner 1 Presented at the 2007 ISPA/SCEA Joint Annual International Conference and Workshop - www.iceaaonline.com Abstract • The upcoming retirement of the Delta II family of launch vehicles leaves a performance gap between small expendable launch vehicles, such as the Pegasus and Taurus, and large vehicles, such as the Delta IV and Atlas V families • This performance gap may lead to a variety of progressions including – large satellites that utilize the full capability of the larger launch vehicles, – medium size satellites that would require dual manifesting on the larger vehicles or – smaller satellites missions that would require a large number of smaller launch vehicles • This paper offers some comparative costs of co-manifesting single- instrument missions on a Delta IV/Atlas V, versus placing several instruments on a larger bus and using a Delta IV/Atlas V, as well as considering smaller, single instrument missions launched on a Minotaur or Taurus • This paper presents the results of a parametric study investigating the cost- effectiveness of different alternatives and their effect on future NASA missions that fall into the Small Explorer (SMEX), Medium Explorer (MIDEX), Earth System Science Pathfinder (ESSP), Discovery, -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Paul Hertz NASA Town Hall with Bonus Material
Paul Hertz Dominic Benford Felicia Chou Valerie Connaughton Lucien Cox Jeanne Davis Kristen Erickson Daniel Evans Michael Garcia Ellen Gertsen Shahid Habib Hashima Hasan Douglas Hudgins Patricia Knezek Elizabeth Landau William Latter Michael New Mario Perez Gregory Robinson Rita Sambruna Evan Scannapieco Kartik Sheth Eric Smith Eric Tollestrup NASA Town Hall with bonus material AAS 235th Meeting | January 5, 2020 Paul Hertz Director, Astrophysics Division Science Mission Directorate @PHertzNASA Posted at http://science.nasa.gov/astrophysics/documents 1 2 Spitzer 8/25/2003 Formulation + SMEX/MO (2025), Implementation MIDEX/MO (2028), etc. Primary Ops ] Extended Ops SXG (RSA) 7/13/2019 Webb Euclid (ESA) 2021 WFIRST 2022 Mid 2020s Ariel (ESA) 2028 XMM-Newton Chandra (ESA) TESS 7/23/1999 12/10/1999 4/18/2018 NuSTAR 6/13/2012 Fermi IXPE Swift 6/11/2008 2021 11/20/2004 XRISM (JAXA) SPHEREx 2022 2023 Hubble ISS-NICER GUSTO 4/24/1990 6/3/2017 2021 SOFIA Full Ops 5/2014 + Athena (early 2030s), Revised November 24, 2019 LISA4 (early 2030s) Outline • Celebrate Accomplishments § Mission Milestones • Committed to Improving § Building an Excellent Workforce § Research and Analysis Initiatives • Program Update § Research & Analysis, Technology, Fellowships § ROSES-2020 Preview • Missions Update § Operating Missions and Senior Review § Webb, WFIRST § Other missions • Planning for the Future § FY20 Budget § Project Artemis § Supporting Astro2020 § Creating the Future 5 NASA Astrophysics Celebrate Accomplishments https://www.nasa.gov/2019 7 NASA Astrophysics -
The Space Infrared Interferometric Telescope (SPIRIT): High- Resolution Imaging and Spectroscopy in the Far-Infrared
Leisawitz, D. et al., J. Adv. Space Res., in press (2007), doi:10.1016/j.asr.2007.05.081 The Space Infrared Interferometric Telescope (SPIRIT): High- resolution imaging and spectroscopy in the far-infrared David Leisawitza, Charles Bakera, Amy Bargerb, Dominic Benforda, Andrew Blainc, Rob Boylea, Richard Brodericka, Jason Budinoffa, John Carpenterc, Richard Caverlya, Phil Chena, Steve Cooleya, Christine Cottinghamd, Julie Crookea, Dave DiPietroa, Mike DiPirroa, Michael Femianoa, Art Ferrera, Jacqueline Fischere, Jonathan P. Gardnera, Lou Hallocka, Kenny Harrisa, Kate Hartmana, Martin Harwitf, Lynne Hillenbrandc, Tupper Hydea, Drew Jonesa, Jim Kellogga, Alan Koguta, Marc Kuchnera, Bill Lawsona, Javier Lechaa, Maria Lechaa, Amy Mainzerg, Jim Manniona, Anthony Martinoa, Paul Masona, John Mathera, Gibran McDonalda, Rick Millsa, Lee Mundyh, Stan Ollendorfa, Joe Pellicciottia, Dave Quinna, Kirk Rheea, Stephen Rineharta, Tim Sauerwinea, Robert Silverberga, Terry Smitha, Gordon Staceyf, H. Philip Stahli, Johannes Staguhn j, Steve Tompkinsa, June Tveekrema, Sheila Walla, and Mark Wilsona a NASA’s Goddard Space Flight Center, Greenbelt, MD b Department of Astronomy, University of Wisconsin, Madison, Wisconsin, USA c California Institute of Technology, Pasadena, CA, USA d Lockheed Martin Technical Operations, Bethesda, Maryland, USA e Naval Research Laboratory, Washington, DC, USA f Department of Astronomy, Cornell University, Ithaca, USA g Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA h Astronomy Department, University of Maryland, College Park, Maryland, USA i NASA’s Marshall Space Flight Center, Huntsville, Alabama, USA j SSAI, Lanham, Maryland, USA ABSTRACT We report results of a recently-completed pre-Formulation Phase study of SPIRIT, a candidate NASA Origins Probe mission. SPIRIT is a spatial and spectral interferometer with an operating wavelength range 25 - 400 µm. -
Special Spitzer Telescope Edition No
INFRARED SCIENCE INTEREST GROUP Special Spitzer Telescope Edition No. 4 | August 2020 Contents From the IR SIG Leadership Council In the time since our last newsletter in January, the world has changed. 1 From the SIG Leadership Travel restrictions and quarantine have necessitated online-conferences, web-based meetings, and working from home. Upturned semesters, constantly shifting deadlines and schedules, and the evolving challenge of Science Highlights keeping our families and communities safe have all taken their toll. We hope this newsletter offers a moment of respite and a reminder that our community 2 Mysteries of Exoplanet continues its work even in the face of great uncertainty and upheaval. Atmospheres In January we said goodbye to the Spitzer Space Telescope, which 4 Relevance of Spitzer in the completed its mission after sixteen years in space. In celebration of Spitzer, Era of Roman, Euclid, and in recognition of the work of so many members of our community, this Rubin & SPHEREx newsletter edition specifically highlights cutting edge science based on and inspired by Spitzer. In the words of Dr. Paul Hertz, Director of Astrophysics 6 Spitzer: The Star-Formation at NASA: Legacy Lives On "Spitzer taught us how important infrared light is to our 8 AKARI Spitzer Survey understanding of our universe, both in our own cosmic 10 Science Impact of SOFIA- neighborhood and as far away as the most distant galaxies. HIRMES Termination The advances we make across many areas in astrophysics in the future will be because of Spitzer's extraordinary legacy." Technical Highlights Though Spitzer is gone, our community remains optimistic and looks forward to the advances that the next generation of IR telescopes will bring. -
Spitzer Space Telescope
Implementing Portals of the Universe: Lessons Learned Spitzer Space Telescope Lisa Storrie-Lombardi Spitzer Science Center, Manager & Asst. Director for Community Affairs Basic Parameters Mission Duration: 8+ years: year 3 of Warm +5.5 yr Cryogenic Mission Userbase: international, thousands Archive Data Volume: > 50 TB, tens of millions of data files Instruments: Warm Mission -- IRAC 3.6 and 4.5 micron imaging Cryogenic Mission: IRAC (3.6 – 8 micron imaging), MIPS (24, 70, 160 micron imaging+ SED mode), IRS (5-40 micron spec. +16 micron imaging) Program Model: 100% GO time for Warm Mission Cryogenic Mission: 80-85% GO, 15-20% GTO + Archive & Theory programs Proposals/Cycle: Warm Mission 150-200 (by design) Cryogenic Mission: 650 – 850 Users: >8,000 PI/CoIs for mission (10% unique), 20% PIs new in Cycle-8 53 Legacy/Exploration Science programs have engaged community in new way Legacy program was pioneered by Spitzer with input from community task force Funding model: Formulaic data analysis funding Warm Mission: $5-10m/cycle GO funding 7000 – 8000 hours/year Cryogenic mission: $20-25m/cycle GO funding 6000 – 6500 hours/year Default proprietary data period: Exploration Science (80% of Warm Mission hrs) – no proprietary period Cryogenic mission – Legacy programs also had zero proprietary period Regular GO programs – 1 year Implementing Portals of the Universe -- 25 April 2012 SPITZER SPACE TELESCOPE 1 Best Practices Implementing Portals of the Universe -- 25 April 2012 SPITZER SPACE TELESCOPE 2 Highlight #1: Major Mission Evolution is Possible*