Chronology of NASA Expendable Vehicle Missions Since 1990
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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. -
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. -
A B 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21
A B 1 Name of Satellite, Alternate Names Country of Operator/Owner 2 AcrimSat (Active Cavity Radiometer Irradiance Monitor) USA 3 Afristar USA 4 Agila 2 (Mabuhay 1) Philippines 5 Akebono (EXOS-D) Japan 6 ALOS (Advanced Land Observing Satellite; Daichi) Japan 7 Alsat-1 Algeria 8 Amazonas Brazil 9 AMC-1 (Americom 1, GE-1) USA 10 AMC-10 (Americom-10, GE 10) USA 11 AMC-11 (Americom-11, GE 11) USA 12 AMC-12 (Americom 12, Worldsat 2) USA 13 AMC-15 (Americom-15) USA 14 AMC-16 (Americom-16) USA 15 AMC-18 (Americom 18) USA 16 AMC-2 (Americom 2, GE-2) USA 17 AMC-23 (Worldsat 3) USA 18 AMC-3 (Americom 3, GE-3) USA 19 AMC-4 (Americom-4, GE-4) USA 20 AMC-5 (Americom-5, GE-5) USA 21 AMC-6 (Americom-6, GE-6) USA 22 AMC-7 (Americom-7, GE-7) USA 23 AMC-8 (Americom-8, GE-8, Aurora 3) USA 24 AMC-9 (Americom 9) USA 25 Amos 1 Israel 26 Amos 2 Israel 27 Amsat-Echo (Oscar 51, AO-51) USA 28 Amsat-Oscar 7 (AO-7) USA 29 Anik F1 Canada 30 Anik F1R Canada 31 Anik F2 Canada 32 Apstar 1 China (PR) 33 Apstar 1A (Apstar 3) China (PR) 34 Apstar 2R (Telstar 10) China (PR) 35 Apstar 6 China (PR) C D 1 Operator/Owner Users 2 NASA Goddard Space Flight Center, Jet Propulsion Laboratory Government 3 WorldSpace Corp. Commercial 4 Mabuhay Philippines Satellite Corp. Commercial 5 Institute of Space and Aeronautical Science, University of Tokyo Civilian Research 6 Earth Observation Research and Application Center/JAXA Japan 7 Centre National des Techniques Spatiales (CNTS) Government 8 Hispamar (subsidiary of Hispasat - Spain) Commercial 9 SES Americom (SES Global) Commercial -
Kicksat: a Crowd-Funded Mission to Demonstrate the World’S Smallest Spacecraft
SSC13-IX-5 KickSat: A Crowd-Funded Mission To Demonstrate The World’s Smallest Spacecraft Zachary Manchester, Mason Peck Cornell University Upson Hall, Ithaca, NY 14853; 607-279-1358 [email protected] Andrew Filo 4Special Projects 22670 Oakcrest Ct, Cupertino, CA 95014; 650-940-1677 [email protected] ABSTRACT Thanks to rapid advances made in the semiconductor industry, it is now possible to integrate most of the features of a traditional spacecraft onto a chip-scale device. The Sprite ChipSat, in development at Cornell since 2008, is an example of such a device. The KickSat mission, scheduled for launch in late 2013, will deploy 128 Sprites in low Earth orbit to test their survivability and demonstrate their code division multiple access (CDMA) communication system. The Sprites are expected to remain in orbit for several days while downlinking telemetry to ground stations before reentry. KickSat has been partially funded by over 300 backers through the crowd-funding website Kickstarter. Reference designs for the Sprites, along with a low-cost ground station receiver, are being made available under an open-source license. INTRODUCTION By dramatically reducing the cost and complexity of The rapid miniaturization of commercial-off-the-shelf building and launching a spacecraft, ChipSats could also help expand access to space for students and (COTS) electronics, driven in recent years by the hobbyists. In the near future, it will be possible for a emergence of smart phones, has made many of the high school science class, amateur radio club, or components used in spacecraft available in very small, motivated hobbyist to choose sensors, assemble a low-cost, low-power packages. -
Status of Chips: a Nasa University Explorer Astronomy Mission
SSC00-V-6 STATUS OF CHIPS: A NASA UNIVERSITY EXPLORER ASTRONOMY MISSION Will Marchant Space Sciences Laboratory - University of California, Berkeley 7962 Leeds Manor Road Marshall, VA 20115-2624 [email protected] Phone: (540) 347-1461 Fax: (954) 301-5786 Dr. Ellen Riddle Taylor DesignNet Engineering Group 275 Liberty Street, #6 San Francisco, CA 94114 [email protected] Phone: (510) 643-4054 Abstract. In the age of "Faster, Better, Cheaper", NASA's Goddard Space Flight Center has been looking for a way to implement university based world class science missions for significantly less money. The University Explorer (UNEX) program is the result. UNEX missions are designed for rapid turnaround with fixed budgets in the $10 million US dollar range. The CHIPS project was selected in 1998. The CHIPS mission has passed the Concept Study and will be having the Confirmation Review in August 2000. Many lessons have already been learned from the CHIPS UNEX project. This paper will discuss the early issues surrounding the use of commercial satellite constellations as the bus and the politics of small satellites using foreign launchers. The difficulties of finding a spacecraft in the UNEX price range will be highlighted. The advantages of utilizing Internet technologies from the earliest phases of the project through to communications with the spacecraft on orbit will be discussed. The current state of the program will be summarized and the project's plans for the future will be charted. What Is UNEX the constraints UNEX program, will provide spectral sky maps of the scientifically critical but The University-Class Explorer (UNEX) program virtually unexplored extreme ultraviolet (EUV) is funded by NASA with the goal of demonstrating band between 90 and 260 Å. -
Chronology of NASA Expendable Vehicle Missions Since 1990
Chronology of NASA Expendable Vehicle Missions Since 1990 Launch Launch Date Payload Vehicle Site1 June 1, 1990 ROSAT (Roentgen Satellite) Delta II ETR, 5:48 p.m. EDT An X-ray observatory developed through a cooperative program between Germany, the U.S., and (Delta 195) LC 17A the United Kingdom. Originally proposed by the Max-Planck-Institut für extraterrestrische Physik (MPE) and designed, built and operated in Germany. Launched into Earth orbit on a U.S. Air Force vehicle. Mission ended after almost nine years, on Feb. 12, 1999. July 25, 1990 CRRES (Combined Radiation and Release Effects Satellite) Atlas I ETR, 3:21 p.m. EDT NASA payload. Launched into a geosynchronous transfer orbit for a nominal three-year mission to (AC-69) LC 36B investigate fields, plasmas, and energetic particles inside the Earth's magnetosphere. Due to onboard battery failure, contact with the spacecraft was lost on Oct. 12, 1991. May 14, 1991 NOAA-D (TIROS) (National Oceanic and Atmospheric Administration-D) Atlas-E WTR, 11:52 a.m. EDT A Television Infrared Observing System (TIROS) satellite. NASA-developed payload; USAF (Atlas 50-E) SLC 4 vehicle. Launched into sun-synchronous polar orbit to allow the satellite to view the Earth's entire surface and cloud cover every 12 hours. Redesignated NOAA-12 once in orbit. June 29, 1991 REX (Radiation Experiment) Scout 216 WTR, 10:00 a.m. EDT USAF payload; NASA vehicle. Launched into 450 nm polar orbit. Designed to study scintillation SLC 5 effects of the Earth's atmosphere on RF transmissions. 114th launch of Scout vehicle. -
Centaur Launches
Centaur Launch Record 1962 -2012 No Veh No Date Failure Payload Launch Vehicle Mgmt. ----------------------------------------------------------------------------------------------------------------------------------- Centaur Developmental Program 1 AC- 1 05.09.1962 F* Centaur AC-1 Atlas-LV3C Centaur-A MSFC 2 AC- 2 11.27.1963 Centaur AC-2 Atlas-LV3C Centaur-B Lewis 3 AC- 3 06.30.1964 F Centaur AC-3 Atlas-LV3C Centaur-C Lewis 4 AC- 4 12.11.1964 Surveyor-Model -1 Atlas-LV3C Centaur-C Lewis 5 AC- 5 03.02.1965 F Surveyor-SD 1 Atlas-LV3C Centaur-C Lewis 6 AC- 6 08.11.1965 Surveyor-SD 2 Atlas-LV3C Centaur-D Lewis 7 AC- 8 04.07.1966 Surveyor-SD 3 Atlas-LV3C Centaur-D Lewis Centaur-D Surveyor Missions 8 AC- 10 05.30.1966 Surveyor 1 Atlas-LV3C Centaur-D Lewis 9 AC- 7 09.20.1966 Surveyor 2 Atlas-LV3C Centaur-D Lewis 10 AC- 9 10.26.1966 Surveyor-SD 4 Atlas-LV3C Centaur-D Lewis 11 AC- 12 04.17.1967 Surveyor 3 Atlas-LV3C Centaur-D Lewis 12 AC- 11 07.14.1967 Surveyor 4 Atlas-LV3C Centaur-D Lewis 13 AC- 13 09.08.1967 Surveyor 5 Atlas-LV3C Centaur-D Lewis 14 AC- 14 11.07.1967 Surveyor 6 Atlas-LV3C Centaur-D Lewis 15 AC- 15 01.07.1968 Surveyor 7 Atlas-LV3C Centaur-D Lewis Centaur-D Spacecraft and Satellites 16 AC- 17 08.10.1968 F ATS 4 Atlas-LV3C Centaur-D Lewis 17 AC- 16 12.07.1968 OAO 2 Atlas-LV3C Centaur-D Lewis 18 AC- 20 02.24.1969 Mariner 6 Atlas-LV3C Centaur-D Lewis 19 AC- 19 03.27.1969 Mariner 7 Atlas-LV3C Centaur-D Lewis 20 AC- 18 08.12.1969 ATS 5 Atlas-LV3C Centaur-D Lewis 21 AC- 21 11.30.1970 F OAO B Atlas-LV3C Centaur-D Lewis 22 AC- 25 01.25.1971 -
Committee on the Societal and Economic Impacts of Severe Space Weather Events: a Workshop
Committee on the Societal and Economic Impacts of Severe Space Weather Events: A Workshop Space Studies Board Division on Engineering and Physical Sciences THE NATIONAL ACADEMIES PRESS 500 Fifth Street, N.W. Washington, DC 20001 NOTICE: The project that is the subject of this report was approved by the Governing Board of the National Research Council, whose members are drawn from the councils of the National Academy of Sciences, the National Academy of Engineering, and the Institute of Medicine. The members of the committee responsible for the report were chosen for their special competences and with regard for appropriate balance. This study is based on work supported by the Contract NASW-01001 between the National Academy of Sciences and the National Aeronautics and Space Administration. Any opinions, findings, conclusions, or recommendations expressed in this pub- lication are those of the author(s) and do not necessarily reflect the views of the agency that provided support for the project. Cover: (Upper left) A looping eruptive prominence blasted out from a powerful active region on July 29, 2005, and within an hour had broken away from the Sun. Active regions are areas of strong magnetic forces. Image courtesy of SOHO, a project of international cooperation between the European Space Agency and NASA. International Standard Book Number 13: 978-0-309-12769-1 International Standard Book Number 10: 0-309-12769-6 Copies of this report are available free of charge from: Space Studies Board National Research Council 500 Fifth Street, N.W. Washington, DC 20001 Additional copies of this report are available from the National Academies Press, 500 Fifth Street, N.W., Lockbox 285, Wash- ington, DC 20055; (800) 624-6242 or (202) 334-3313 (in the Washington metropolitan area); Internet, http://www.nap.edu. -
From the Geostationary Ring
Preprints (www.preprints.org) | NOT PEER-REVIEWED | Posted: 3 November 2020 doi:10.20944/preprints202009.0629.v2 Article GEO-GEO Stereo-Tracking of Atmospheric Motion Vectors (AMVs) from the Geostationary Ring James L. Carr 1,* , Dong L. Wu 2 , Jaime Daniels 3 , Mariel D. Friberg 2,4 , Wayne Bresky 5 and Houria Madani 1 1 Carr Astronautics, 6404 Ivy Lane, Suite 333, Greenbelt, MD 20770, USA; [email protected] 2 NASA Goddard Space Flight Center, Greenbelt, MD 20770, USA; [email protected] 3 NOAA/NESDIS Center for Satellite Applications and Research, College Park, MD 20740, USA 4 Universities Space Research Association, Columbia, MD 21046, USA 5 I.M. Systems Group (IMSG), Rockville, MD 20852, USA * Correspondence: [email protected] Abstract: Height assignment is an important problem for satellite measurements of Atmospheric Motion Vectors (AMVs) that are interpreted as winds by forecast and assimilation systems. Stereo methods assign heights to AMVs from the parallax observed between observations from different vantage points in orbit while tracking cloud or moisture features. In this paper, we fully develop the stereo method to jointly retrieve wind vectors with their geometric heights from geostationary satellite pairs. Synchronization of observations between observing systems is not required. NASA and NOAA stereo-winds codes have implemented this method and we have processed large datasets from GOES-16, -17, and Himawari-8. Our retrievals are validated against rawinsonde observations and demonstrate the potential to improve forecast skill. Stereo winds also offer an important mitigation for the loop heat pipe anomaly on GOES-17 during times when warm focal plane temperatures cause infra-red channels that are needed for operational height assignments to fail. -
Index of Astronomia Nova
Index of Astronomia Nova Index of Astronomia Nova. M. Capderou, Handbook of Satellite Orbits: From Kepler to GPS, 883 DOI 10.1007/978-3-319-03416-4, © Springer International Publishing Switzerland 2014 Bibliography Books are classified in sections according to the main themes covered in this work, and arranged chronologically within each section. General Mechanics and Geodesy 1. H. Goldstein. Classical Mechanics, Addison-Wesley, Cambridge, Mass., 1956 2. L. Landau & E. Lifchitz. Mechanics (Course of Theoretical Physics),Vol.1, Mir, Moscow, 1966, Butterworth–Heinemann 3rd edn., 1976 3. W.M. Kaula. Theory of Satellite Geodesy, Blaisdell Publ., Waltham, Mass., 1966 4. J.-J. Levallois. G´eod´esie g´en´erale, Vols. 1, 2, 3, Eyrolles, Paris, 1969, 1970 5. J.-J. Levallois & J. Kovalevsky. G´eod´esie g´en´erale,Vol.4:G´eod´esie spatiale, Eyrolles, Paris, 1970 6. G. Bomford. Geodesy, 4th edn., Clarendon Press, Oxford, 1980 7. J.-C. Husson, A. Cazenave, J.-F. Minster (Eds.). Internal Geophysics and Space, CNES/Cepadues-Editions, Toulouse, 1985 8. V.I. Arnold. Mathematical Methods of Classical Mechanics, Graduate Texts in Mathematics (60), Springer-Verlag, Berlin, 1989 9. W. Torge. Geodesy, Walter de Gruyter, Berlin, 1991 10. G. Seeber. Satellite Geodesy, Walter de Gruyter, Berlin, 1993 11. E.W. Grafarend, F.W. Krumm, V.S. Schwarze (Eds.). Geodesy: The Challenge of the 3rd Millennium, Springer, Berlin, 2003 12. H. Stephani. Relativity: An Introduction to Special and General Relativity,Cam- bridge University Press, Cambridge, 2004 13. G. Schubert (Ed.). Treatise on Geodephysics,Vol.3:Geodesy, Elsevier, Oxford, 2007 14. D.D. McCarthy, P.K. -
Chips: a Nasa University Explorer Astronomy Mission
SSC03-V-3 CHIPS: A NASA UNIVERSITY EXPLORER ASTRONOMY MISSION Ellen Taylor DesignNet Engineering Group San Francisco, CA 94114 Mark Hurwitz, Will Marchant, Michael Sholl Space Sciences Laboratory - University of California, Berkeley Berkeley, CA 94720-7450 Simon Dawson, Jeff Janicik, Jonathan Wolff SpaceDev, Inc Poway, CA 92064 Abstract. On January 12th, 2003, the Cosmic Hot Interstellar Plasma Spectrometer Spacecraft (CHIPSat) launched successfully from Vandenberg Air Force Base as a secondary payload on a Delta II booster. CHIPSat completed commissioning in February 2003, and is now a fully operational observatory. The main science objective is to measure extreme ultraviolet emissions from the interstellar medium. Data on the distribution and intensity of these emissions allow scientists to test competing theories on the formation of hot interstellar gas clouds surrounding our solar system. CHIPSat is the first satellite in NASA's University-class Explorers Program (UNEX) to make it to orbit. The UNEX program was conceived by NASA as a new class of explorer mission charged with demonstrating that significant science and/or technology experiments can be performed with small satellites, constrained budgets and limited schedules. This paper presents the CHIPSat design, discusses the on-orbit performance to date, and provides lessons learned throughout the project. Introduction regions of particular interest long enough to provide the signal to noise ratio (S/N) detection The Cosmic Hot Interstellar Plasma required for the strongest emission lines. Many Spectrometer spacecraft (CHIPSat), the first of of these regions, at the galactic pole, have been NASA's streamlined University-Class Explorer observed to a depth of about 300,000 seconds missions, was launched out of Vandenberg Air per resolution element (resel).