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The Space Impact of the Euro Crisis 50 Years After Mariner 2: Exploration at a Crossroads
0827_SPN_DOM_00_019_00 (READ ONLY) 8/24/2012 11:39 AM Page 19 www.spacenews.com SPACENEWS 19 August27, 2012 TheSpaceImpact of the Euro Crisis < ROBBIN LAIRD and HARALD MALMGREN > he European sovereign debt crisis Europe will now be challenged in the ing to hide the reality of European bank of the savings of millions of European is not simply abump in historical form of rollbacks of the many inter- weaknesses. The main reason is that eu- citizens. Tprogress; it is the end of aperiod twined strands of integration, fraying rozone economies are far more bank- European leaders are also attempt- of historyand acritical point in Euro- what has been an intricate but incom- dependent than economies like those in ing to initiate amore comprehensive fis- pean and global transition in the 21st plete tapestry. It is questionable whether the United States or United Kingdom, cal union, with new decision-making century. Europe will be able to prevent stalling of where substantial nonbank financing al- mechanisms that transfer sovereignty in The confluence of several trend lines the integration process in the face of ternatives exist for the corporate sector. parallel with the new banking union. We — the unification of Germany,the end widening gaps among the interests of In the eurozone, banks are the fi- do not believe that any of the eurozone of the Soviet Union, the collapse of the each nation and even within each nation. nancial markets; in the U.S., banks are governments are ready for such apoliti- Berlin Wall, the expansion of NATO, Since the birth of the euro, the but one segment of amultifaceted fi- cal transition in which citizens in each the expansion of the European Union French and Germans were in the lead in nancial market. -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
Trans-Neptunian Objects a Brief History, Dynamical Structure, and Characteristics of Its Inhabitants
Trans-Neptunian Objects A Brief history, Dynamical Structure, and Characteristics of its Inhabitants John Stansberry Space Telescope Science Institute IAC Winter School 2016 IAC Winter School 2016 -- Kuiper Belt Overview -- J. Stansberry 1 The Solar System beyond Neptune: History • 1930: Pluto discovered – Photographic survey for Planet X • Directed by Percival Lowell (Lowell Observatory, Flagstaff, Arizona) • Efforts from 1905 – 1929 were fruitless • discovered by Clyde Tombaugh, Feb. 1930 (33 cm refractor) – Survey continued into 1943 • Kuiper, or Edgeworth-Kuiper, Belt? – 1950’s: Pluto represented (K.E.), or had scattered (G.K.) a primordial, population of small bodies – thus KBOs or EKBOs – J. Fernandez (1980, MNRAS 192) did pretty clearly predict something similar to the trans-Neptunian belt of objects – Trans-Neptunian Objects (TNOs), trans-Neptunian region best? – See http://www2.ess.ucla.edu/~jewitt/kb/gerard.html IAC Winter School 2016 -- Kuiper Belt Overview -- J. Stansberry 2 The Solar System beyond Neptune: History • 1978: Pluto’s moon, Charon, discovered – Photographic astrometry survey • 61” (155 cm) reflector • James Christy (Naval Observatory, Flagstaff) – Technologically, discovery was possible decades earlier • Saturation of Pluto images masked the presence of Charon • 1988: Discovery of Pluto’s atmosphere – Stellar occultation • Kuiper airborne observatory (KAO: 90 cm) + 7 sites • Measured atmospheric refractivity vs. height • Spectroscopy suggested N2 would dominate P(z), T(z) • 1992: Pluto’s orbit explained • Outward migration by Neptune results in capture into 3:2 resonance • Pluto’s inclination implies Neptune migrated outward ~5 AU IAC Winter School 2016 -- Kuiper Belt Overview -- J. Stansberry 3 The Solar System beyond Neptune: History • 1992: Discovery of 2nd TNO • 1976 – 92: Multiple dedicated surveys for small (mV > 20) TNOs • Fall 1992: Jewitt and Luu discover 1992 QB1 – Orbit confirmed as ~circular, trans-Neptunian in 1993 • 1993 – 4: 5 more TNOs discovered • c. -
Glossary Glossary
Glossary Glossary Albedo A measure of an object’s reflectivity. A pure white reflecting surface has an albedo of 1.0 (100%). A pitch-black, nonreflecting surface has an albedo of 0.0. The Moon is a fairly dark object with a combined albedo of 0.07 (reflecting 7% of the sunlight that falls upon it). The albedo range of the lunar maria is between 0.05 and 0.08. The brighter highlands have an albedo range from 0.09 to 0.15. Anorthosite Rocks rich in the mineral feldspar, making up much of the Moon’s bright highland regions. Aperture The diameter of a telescope’s objective lens or primary mirror. Apogee The point in the Moon’s orbit where it is furthest from the Earth. At apogee, the Moon can reach a maximum distance of 406,700 km from the Earth. Apollo The manned lunar program of the United States. Between July 1969 and December 1972, six Apollo missions landed on the Moon, allowing a total of 12 astronauts to explore its surface. Asteroid A minor planet. A large solid body of rock in orbit around the Sun. Banded crater A crater that displays dusky linear tracts on its inner walls and/or floor. 250 Basalt A dark, fine-grained volcanic rock, low in silicon, with a low viscosity. Basaltic material fills many of the Moon’s major basins, especially on the near side. Glossary Basin A very large circular impact structure (usually comprising multiple concentric rings) that usually displays some degree of flooding with lava. The largest and most conspicuous lava- flooded basins on the Moon are found on the near side, and most are filled to their outer edges with mare basalts. -
Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M. -
Markov Chain Monte-Carlo Orbit Computation for Binary Asteroids
SF2A 2013 L. Cambr´esy,F. Martins, E. Nuss and A. Palacios (eds) MARKOV CHAIN MONTE-CARLO ORBIT COMPUTATION FOR BINARY ASTEROIDS Dagmara Oszkiewicz2; 1, Daniel Hestroffer2 and Pedro David2 Abstract. We present a novel method of orbit computation for resolved binary asteroids. The method combines the Thiele, Innes, van den Bos method with a Markov chain Monte Carlo technique (MCMC). The classical Thiele-van den Bos method has been commonly used in multiple applications before, including orbits of binary stars and asteroids; conversely this novel method can be used for the analysis of binary stars, and of other gravitationally bound binaries. The method requires a minimum of three observations (observing times and relative positions - Cartesian or polar) made at the same tangent plane - or close enough for enabling a first approximation. Further, the use of the MCMC technique for statistical inversion yields the whole bundle of possible orbits, including the one that is most probable. In this new method, we make use of the Metropolis-Hastings algorithm to sample the parameters of the Thiele-van den Bos method, that is the orbital period (or equivalently the double areal constant) together with three randomly selected observations from the same tangent plane. The observations are sampled within their observational errors (with an assumed distribution) and the orbital period is the only parameter that has to be tuned during the sampling procedure. We run multiple chains to ensure that the parameter phase space is well sampled and that the solutions have converged. After the sampling is completed we perform convergence diagnostics. The main advantage of the novel approach is that the orbital period does not need to be known in advance and the entire region of possible orbital solutions is sampled resulting in a maximum likelihood solution and the confidence regions. -
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Five New and Three Improved Mutual Orbits of Transneptunian Binaries W.M. Grundya, K.S. Nollb, F. Nimmoc, H.G. Roea, M.W. Buied, S.B. Portera, S.D. Benecchie,f, D.C. Stephensg, H.F. Levisond, and J.A. Stansberryh a. Lowell Observatory, 1400 W. Mars Hill Rd., Flagstaff AZ 86001. b. Space Telescope Science Institute, 3700 San Martin Dr., Baltimore MD 21218. c. Department of Earth and Planetary Sciences, University of California, Santa Cruz CA 95064. d. Southwest Research Institute, 1050 Walnut St. #300, Boulder CO 80302. e. Planetary Science Institute, 1700 E. Fort Lowell, Suite 106, Tucson AZ 85719. f. Carnegie Institution of Washington, Department of Terrestrial Magnetism, 5241 Broad Branch Rd. NW, Washington DC 20015. g. Dept. of Physics and Astronomy, Brigham Young University, N283 ESC Provo UT 84602. h. Steward Observatory, University of Arizona, 933 N. Cherry Ave., Tucson AZ 85721. — Published in 2011: Icarus 213, 678-692. — doi:10.1016/j.icarus.2011.03.012 ABSTRACT We present three improved and five new mutual orbits of transneptunian binary systems (58534) Logos-Zoe, (66652) Borasisi-Pabu, (88611) Teharonhiawako-Sawiskera, (123509) 2000 WK183, (149780) Altjira, 2001 QY297, 2003 QW111, and 2003 QY90 based on Hubble Space Tele- scope and Keck II laser guide star adaptive optics observations. Combining the five new orbit solutions with 17 previously known orbits yields a sample of 22 mutual orbits for which the period P, semimajor axis a, and eccentricity e have been determined. These orbits have mutual periods ranging from 5 to over 800 days, semimajor axes ranging from 1,600 to 37,000 km, ec- centricities ranging from 0 to 0.8, and system masses ranging from 2 × 1017 to 2 × 1022 kg. -
Mariner to Mercury, Venus and Mars
NASA Facts National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, CA 91109 Mariner to Mercury, Venus and Mars Between 1962 and late 1973, NASA’s Jet carry a host of scientific instruments. Some of the Propulsion Laboratory designed and built 10 space- instruments, such as cameras, would need to be point- craft named Mariner to explore the inner solar system ed at the target body it was studying. Other instru- -- visiting the planets Venus, Mars and Mercury for ments were non-directional and studied phenomena the first time, and returning to Venus and Mars for such as magnetic fields and charged particles. JPL additional close observations. The final mission in the engineers proposed to make the Mariners “three-axis- series, Mariner 10, flew past Venus before going on to stabilized,” meaning that unlike other space probes encounter Mercury, after which it returned to Mercury they would not spin. for a total of three flybys. The next-to-last, Mariner Each of the Mariner projects was designed to have 9, became the first ever to orbit another planet when two spacecraft launched on separate rockets, in case it rached Mars for about a year of mapping and mea- of difficulties with the nearly untried launch vehicles. surement. Mariner 1, Mariner 3, and Mariner 8 were in fact lost The Mariners were all relatively small robotic during launch, but their backups were successful. No explorers, each launched on an Atlas rocket with Mariners were lost in later flight to their destination either an Agena or Centaur upper-stage booster, and planets or before completing their scientific missions. -
Grin,Yaue T: M, 2
4 w .. -. I 1 . National Aeronautics and STace Administration Goddard Space Flight Center C ont r ac t No NAS -5 -f 7 60 THE OUTERMOST BELT OF CFLARGED PARTICLES _- .- - by K. I, Grin,yaue t: M, 2. I~alOkhlOV cussa 3 GPO PRICE $ CFSTI PRICE(S) $ 17 NOVEbI3ER 1965 Hard copy (HC) .J d-0 Microfiche (M F) ,J3’ ff 853 July 85 Issl. kosniicheskogo prostrznstva by K. N. Gringaua Trudy Vsesoyuzrloy koneferentsii & M. z. Khokhlov po kosaiches?%inlucham, 467 - 482 Noscon, June 1965. This report deals with the result of the study of a eone of char- ged pxticles with comparatively low ener-ies (from -100 ev to 10 - 4Okev), situated beyond the outer rzdiation belt (including the new data obtained on Ilectron-2 and Zond-2). 'The cutkors review, first of all, an2 in chronolo~icalorder, the space probes on which data on soft electrons 'and protons were obtained beyond the rsdistion belts. A brief review is given of soae examples of regis- tration of soft electrons at high geominetic latitudes by Mars-1 and Elec- tron-2. It is shown that here, BS in other space probes, the zones of soft electron flwcys are gartly overlap7inr with the zones of trapped radiation. The spatial distributio;: of fluxcs of soft electrons is sixdied in liqht of data oStziined fro.1 various sFnce probes, such as Lunik-1, Explorer-12, Explorer-18, for the daytime rerion along the map-etosphere boundary &om the sumy side. The night re-ion of fluxes is exmined fron data provided by Lunik-2, 7xpiorer-12, Z~nd-2~~ni the results of various latest works with reKarr! to the relationshi- of that distribution with the structure of tire marnetic field are exCmined and cornpcved. -
The Flight Plan
M A R C H 2 0 2 1 THE FLIGHT PLAN The Newsletter of AIAA Albuquerque Section The American Institute of Aeronautics and Astronautics AIAA ALBUQUERQUE MARCH 2021 SECTION MEETING: MAKING A DIFFERENCE A T M A C H 2 . Presenter. Lt. Col. Tucker Hamilton Organization USAF F-35 Developmental Test Director of Operations INSIDE THIS ISSUE: Abstract I humbly present my flying experiences through SECTION CALENDAR 2 pictures and videos of what it takes and what it is like to be an Experimental Fighter Test Pilot. My personal stories include NATIONAL AIAA EVENTS 2 major life-threatening aircraft accidents, close saves, combat SPACE NUCLEAR PROPULSION REPORT 3 flying revelations, serendipitous opportunities testing first of its kind technology, flying over 30 aircraft from a zeppelin to a ALBUQUERQUE DECEMBER MEETING 5 MiG-15 to an A-10, and managing the Joint Strike Fighter De- velopmental Test program for all three services. Through ALBUQUERQUE JANUARY MEETING 6 these experiences you will learn not just what a Test Pilot does, but also gain encour- ALBUQUERQUE FEBRUARY MEETING 7 agement through my lessons learned on how to make a difference in your local com- munities…did I mention cool flight test videos! CALL FOR SCIENCE FAIR JUDGES 9 Lt Col Tucker "Cinco" Hamilton started his Air Force career as an CALL FOR SCHOLARSHIP APPLICATIONS 10 operational F-15C pilot. He supported multiple Red Flag Exercises and real world Operation Noble Eagle missions where he protect- NEW AIAA HIGH SCHOOL MEMBERSHIPS 10 ed the President of the United States; at times escorting Air Force One. -
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. -
Comparative Kbology: Using Surface Spectra of Triton
COMPARATIVE KBOLOGY: USING SURFACE SPECTRA OF TRITON, PLUTO, AND CHARON TO INVESTIGATE ATMOSPHERIC, SURFACE, AND INTERIOR PROCESSES ON KUIPER BELT OBJECTS by BRYAN JASON HOLLER B.S., Astronomy (High Honors), University of Maryland, College Park, 2012 B.S., Physics, University of Maryland, College Park, 2012 M.S., Astronomy, University of Colorado, 2015 A thesis submitted to the Faculty of the Graduate School of the University of Colorado in partial fulfillment of the requirement for the degree of Doctor of Philosophy Department of Astrophysical and Planetary Sciences 2016 This thesis entitled: Comparative KBOlogy: Using spectra of Triton, Pluto, and Charon to investigate atmospheric, surface, and interior processes on KBOs written by Bryan Jason Holler has been approved for the Department of Astrophysical and Planetary Sciences Dr. Leslie Young Dr. Fran Bagenal Date The final copy of this thesis has been examined by the signatories, and we find that both the content and the form meet acceptable presentation standards of scholarly work in the above mentioned discipline. ii ABSTRACT Holler, Bryan Jason (Ph.D., Astrophysical and Planetary Sciences) Comparative KBOlogy: Using spectra of Triton, Pluto, and Charon to investigate atmospheric, surface, and interior processes on KBOs Thesis directed by Dr. Leslie Young This thesis presents analyses of the surface compositions of the icy outer Solar System objects Triton, Pluto, and Charon. Pluto and its satellite Charon are Kuiper Belt Objects (KBOs) while Triton, the largest of Neptune’s satellites, is a former member of the KBO population. Near-infrared spectra of Triton and Pluto were obtained over the previous 10+ years with the SpeX instrument at the IRTF and of Charon in Summer 2015 with the OSIRIS instrument at Keck.