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Cross & Cockade International SERIALS with PHOTOGRAPHS
Cross & Cockade International THE FIRST WORLD WAR AVIATION HISTORICAL SOCIETY Registered Charity No 1117741 www.crossandcockade.com INDEX for SERIALS with PHOTOGRAPHS This is a provisional index of all the photographs of aircraft with serial numbers in the 46 years of the Cross & Cockade Journal. There are only photographs with identifiable serials, no other items are indexed. Following the Aircraft serial number is the make & model in parentheses, then page number format is: first the volume number, followed by the issue number (1 to 4) between periods with the page number(s) at the end. The cover pages use the last three characters with a 'c' (cover) 'f' - 'r'(front-rear), '1'(outside) '2' (inside). There are over 4180 entries in three categories, British individual aircraft, other countries individual aircraft, followed by airships & balloons. Regretfully, copies of the photographs are not available. Derek Riley, Jan. 22, 2017 AIRCRAFT SERIAL, BRITISH INDIVIDUAL...............................pg 01 AIRCRAFT SERIALS, OTHER COUNTRY...................................pg 13 AIRSHIPS & BALLOONS.............................................................pg 18 AIRCRAFT SERIAL, British individual 81 (Short Folder Seaplane) 07.1.024, 184 (Short Admiralty Type 184) 04.1.cr2, Serial Aircraft type Page num 07.1.027, 15.4.162 06.4.152, 06.4.cf1, 15.4.166, 16.2.064 2 (Short Biplane) 15.4.148 88 (Borel Seaplane) 15.4.167, 16.2.056 187 (Wight Twin Seaplane) 16.2.065 9 (Etrich Taube Monoplane) 15.4.149, 95 (M.Farman Seaplane) 03.4.139, 16.2.057 201 (RAF BE1) 08.4.150, 36.4.256, 42.3.149 46.4.266 97 (H.Farman Biplane) 16.2.057 202 (Bréguet L.2 biplane) 08.4.149 10 (Short Improved S41 Type) 23.4.171, 98 (H.Farman Biplane) 15.4.157 203 (RAF BE3) 08.4.152, 09.4.172, 20.3.134, 34.1.065 103 (Sopwith Tractor Biplane) 15.4.157, 20.3.135, 23.4.169, 28.4.182, 38.4.239, 14 (Bristol Coanda monoplane) 45.3.176 15.4.165 38.4.242, 41.3.162 16 (Avro 503) 15.4.150 104 (Sopwith Tractor Biplane) 03.4.143 204 (RAF BE4) 20.3.134, 23.4.176, 36.1.058 17 (Hydro Recon. -
The Evolution of a Heterogeneous Martian Mantle: Clues from K, P, Ti, Cr, and Ni Variations in Gusev Basalts and Shergottite Meteorites
Earth and Planetary Science Letters 296 (2010) 67–77 Contents lists available at ScienceDirect Earth and Planetary Science Letters journal homepage: www.elsevier.com/locate/epsl The evolution of a heterogeneous Martian mantle: Clues from K, P, Ti, Cr, and Ni variations in Gusev basalts and shergottite meteorites Mariek E. Schmidt a,⁎, Timothy J. McCoy b a Dept. of Earth Sciences, Brock University, St. Catharines, ON, Canada L2S 3A1 b Dept. of Mineral Sciences, National Museum of Natural History, Smithsonian Institution, Washington, DC 20560-0119, USA article info abstract Article history: Martian basalts represent samples of the interior of the planet, and their composition reflects their source at Received 10 December 2009 the time of extraction as well as later igneous processes that affected them. To better understand the Received in revised form 16 April 2010 composition and evolution of Mars, we compare whole rock compositions of basaltic shergottitic meteorites Accepted 21 April 2010 and basaltic lavas examined by the Spirit Mars Exploration Rover in Gusev Crater. Concentrations range from Available online 2 June 2010 K-poor (as low as 0.02 wt.% K2O) in the shergottites to K-rich (up to 1.2 wt.% K2O) in basalts from the Editor: R.W. Carlson Columbia Hills (CH) of Gusev Crater; the Adirondack basalts from the Gusev Plains have more intermediate concentrations of K2O (0.16 wt.% to below detection limit). The compositional dataset for the Gusev basalts is Keywords: more limited than for the shergottites, but it includes the minor elements K, P, Ti, Cr, and Ni, whose behavior Mars igneous processes during mantle melting varies from very incompatible (prefers melt) to very compatible (remains in the shergottites residuum). -
Airwork Limited
AN APPRECIATION The Council of the Royal Aeronautical Society wish to thank those Companies who, by their generous co-operation, have done so much to help in the production of the Journal ACCLES & POLLOCK LIMITED AIRWORK LIMITED _5£ f» g AIRWORK LIMITED AEROPLANE & MOTOR ALUMINIUM ALVIS LIMITED CASTINGS LTD. ALUMINIUM CASTINGS ^-^rr AIRCRAFT MATERIALS LIMITED ARMSTRONG SIDDELEY MOTORS LTD. STRUCTURAL MATERIALS ARMSTRONG SIDDELEY and COMPONENTS AIRSPEED LIMITED SIR W. G. ARMSTRONG WHITWORTH AIRCRAFT LTD. SIR W. G. ARMSTRONG WHITWORTH AIRCRAFT LIMITED AUSTER AIRCRAFT LIMITED BLACKBURN AIRCRAFT LTD. ^%N AUSTER Blackburn I AIRCRAFT I AUTOMOTIVE PRODUCTS COMPANY LTD. JAMES BOOTH & COMPANY LTD. (H1GH PRECISION! HYDRAULICS a;) I DURALUMIN LJOC kneed *(6>S'f*ir> tttaot • AVIMO LIMITED BOULTON PAUL AIRCRAFT L"TD. OPTICAL - MECHANICAL - ELECTRICAL INSTRUMENTS AERONAUTICAL EQUIPMENT BAKELITE LIMITED BRAKE LININGS LIMITED BAKELITE d> PLASTICS KEGD. TEAM MARKS ilMilNIICI1TIIH I BRAKE AND CLUTCH LININGS T. M. BIRKETT & SONS LTD. THE BRISTOL AEROPLANE CO., LTD. NON-FERROUS CASTINGS AND MACHINED PARTS HANLEY - - STAFFS THE BRITISH ALUMINIUM CO., LTD. BRITISH WIRE PRODUCTS LTD. THE BRITISH AVIATION INSURANCE CO. LTD. BROOM & WADE LTD. iy:i:M.mnr*jy BRITISH AVIATION SERVICES LTD. BRITISH INSULATED CALLENDER'S CABLES LTD. BROWN BROTHERS (AIRCRAFT) LTD. SMS^MMM BRITISH OVERSEAS AIRWAYS CORPORATION BUTLERS LIMITED AUTOMOBILE, AIRCRAFT AND MARITIME LAMPS BOM SEARCHLICHTS AND MOTOR ACCESSORIES BRITISH THOMSON-HOUSTON CO., THE CHLORIDE ELECTRICAL STORAGE CO. LTD. LIMITED (THE) Hxtie AIRCRAFT BATTERIES! Magnetos and Electrical Equipment COOPER & CO. (B'HAM) LTD. DUNFORD & ELLIOTT (SHEFFIELD) LTD. COOPERS I IDBSHU l Bala i IIIIKTI A. C. COSSOR LIMITED DUNLOP RUBBER CO., LTD. -
Book Tribute to George Low –“The Ultimate Engineer”
Book Tribute to George Low –“The Ultimate Engineer” The Ultimate Engineer: The Remarkable Life of NASA's Visionary Leader George M. Low by Richard Jurek Foreword by Gerald D. Griffin From the late 1950s to 1976 the U.S. manned spaceflight program advanced as it did largely due to the extraordinary efforts of Austrian immigrant George M. Low. Described as the "ultimate engineer" during his career at NASA, Low was a visionary architect and leader from the agency's inception in 1958 to his retirement in 1976. As chief of manned spaceflight at NASA, Low was instrumental in the Mercury, Gemini, and Apollo programs. Low's pioneering work paved the way for President Kennedy's decision to make a lunar landing NASA's primary goal in the 1960s. After the tragic 1967 Apollo I fire that took the lives of three astronauts and almost crippled the program, Low took charge of the redesign of the Apollo spacecraft, and helped lead the program from disaster and toward the moon. In 1968, Low made the bold decision to go for lunar orbit on Apollo 8 before the lunar module was ready for flight and after only one Earth orbit test flight of the Command and Service modules. Under Low there were five manned missions, including Apollo 11, the first manned lunar landing. Low's clandestine negotiations with the Soviet Union resulted in a historic joint mission in 1975 that was the precursor to the Shuttle-MIR and International Space Station programs. At the end of his NASA career, Low was one of the leading figures in the development of the Space Shuttle in the early1970s, and was instrumental in NASA's transition into a post-Apollo world. -
Evidence for Thermal-Stress-Induced Rockfalls on Mars Impact Crater Slopes
Icarus 342 (2020) 113503 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Evidence for thermal-stress-induced rockfalls on Mars impact crater slopes P.-A. Tesson a,b,*, S.J. Conway b, N. Mangold b, J. Ciazela a, S.R. Lewis c, D. M�ege a a Space Research Centre, Polish Academy of Science, Wrocław, Poland b Laboratoire de Plan�etologie et G�eodynamique UMR 6112, CNRS, Nantes, France c School of Physical Sciences, The Open University, Walton Hall, Milton Keynes MK7 6AA, UK ARTICLE INFO ABSTRACT Keywords: Here we study rocks falling from exposed outcrops of bedrock, which have left tracks on the slope over which Mars, surface they have bounced and/or rolled, in fresh impact craters (1–10 km in diameter) on Mars. The presence of these Thermal stress tracks shows that these rocks have fallen relatively recently because aeolian processes are known to infill Ices topographic lows over time. Mapping of rockfall tracks indicate trends in frequency with orientation, which in Solar radiation � � turn depend on the latitudinal position of the crater. Craters in the equatorial belt (between 15 N and 15 S) Weathering exhibit higher frequencies of rockfall on their north-south oriented slopes compared to their east-west ones. � Craters >15 N/S have notably higher frequencies on their equator-facing slopes as opposed to the other ori entations. We computed solar radiation on the surface of crater slopes to compare insolation patterns with the spatial distribution of rockfalls, and found statistically significant correlations between maximum diurnal inso lation and rockfall frequency. -
Chapter 6.Qxd
CHAPTER 6: The NASA Family The melding of all of the NASA centers, contractors, universities, and often strong personalities associated with each of them into the productive and efficient organization necessary to complete NASA’s space missions became both more critical and more difficult as NASA turned its attention from Gemini to Apollo. The approach and style and, indeed, the personality of each NASA center differed sharply. The Manned Spacecraft Center was distinctive among all the rest. Fortune magazine suggested in 1967 that the scale of NASA’s operation required a whole new approach and style of management: “To master such massively complex and expensive problems, the agency has mobilized some 20,000 individual firms, more than 400,000 workers, and 200 colleges and universities in a combine of the most advanced resources of American civilization.” The author referred to some of the eight NASA centers and assorted field installations as “pockets of sovereignty” which exercised an enormous degree of independence and autonomy.1 An enduring part of the management problem throughout the Mercury and Gemini programs that became compounded under Apollo, because of its greater technical challenges, was the diversity and distinctiveness of each of the NASA centers. The diverse cultures and capabilities represented by each of the centers were at once the space program’s greatest resource and its Achilles’ heel. NASA was a hybrid organization. At its heart was Langley Memorial Aeronautical Laboratory established by Congress in 1917 near Hampton, Virginia, and formally dedicated in 1920. It became the Langley Research Center. Langley created the Ames Aeronautical Laboratory at Moffett Field, California, in 1939. -
Martian Crater Morphology
ANALYSIS OF THE DEPTH-DIAMETER RELATIONSHIP OF MARTIAN CRATERS A Capstone Experience Thesis Presented by Jared Howenstine Completion Date: May 2006 Approved By: Professor M. Darby Dyar, Astronomy Professor Christopher Condit, Geology Professor Judith Young, Astronomy Abstract Title: Analysis of the Depth-Diameter Relationship of Martian Craters Author: Jared Howenstine, Astronomy Approved By: Judith Young, Astronomy Approved By: M. Darby Dyar, Astronomy Approved By: Christopher Condit, Geology CE Type: Departmental Honors Project Using a gridded version of maritan topography with the computer program Gridview, this project studied the depth-diameter relationship of martian impact craters. The work encompasses 361 profiles of impacts with diameters larger than 15 kilometers and is a continuation of work that was started at the Lunar and Planetary Institute in Houston, Texas under the guidance of Dr. Walter S. Keifer. Using the most ‘pristine,’ or deepest craters in the data a depth-diameter relationship was determined: d = 0.610D 0.327 , where d is the depth of the crater and D is the diameter of the crater, both in kilometers. This relationship can then be used to estimate the theoretical depth of any impact radius, and therefore can be used to estimate the pristine shape of the crater. With a depth-diameter ratio for a particular crater, the measured depth can then be compared to this theoretical value and an estimate of the amount of material within the crater, or fill, can then be calculated. The data includes 140 named impact craters, 3 basins, and 218 other impacts. The named data encompasses all named impact structures of greater than 100 kilometers in diameter. -
11 Fall Unamagazine
FALL 2011 • VOLUME 19 • No. 3 FOR ALUMNI AND FRIENDS OF THE UNIVERSITY OF NORTH ALABAMA Cover Story 10 ..... Thanks a Million, Harvey Robbins Features 3 ..... The Transition 14 ..... From Zero to Infinity 16 ..... Something Special 20 ..... The Sounds of the Pride 28 ..... Southern Laughs 30 ..... Academic Affairs Awards 33 ..... Excellence in Teaching Award 34 ..... China 38 ..... Words on the Breeze Departments 2 ..... President’s Message 6 ..... Around the Campus 45 ..... Class Notes 47 ..... In Memory FALL 2011 • VOLUME 19 • No. 3 for alumni and friends of the University of North Alabama president’s message ADMINISTRATION William G. Cale, Jr. President William G. Cale, Jr. The annual everyone to attend one of these. You may Vice President for Academic Affairs/Provost Handy festival contact Dr. Alan Medders (Vice President John Thornell is drawing large for Advancement, [email protected]) Vice President for Business and Financial Affairs crowds to the many or Mr. Mark Linder (Director of Athletics, Steve Smith venues where music [email protected]) for information or to Vice President for Student Affairs is being played. At arrange a meeting for your group. David Shields this time of year Sometimes we measure success by Vice President for University Advancement William G. Cale, Jr. it is impossible the things we can see, like a new building. Alan Medders to go anywhere More often, though, success happens one Vice Provost for International Affairs in town and not hear music. The festival student at a time as we provide more and Chunsheng Zhang is also a reminder that we are less than better educational opportunities. -
Widespread Crater-Related Pitted Materials on Mars: Further Evidence for the Role of Target Volatiles During the Impact Process ⇑ Livio L
Icarus 220 (2012) 348–368 Contents lists available at SciVerse ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Widespread crater-related pitted materials on Mars: Further evidence for the role of target volatiles during the impact process ⇑ Livio L. Tornabene a, , Gordon R. Osinski a, Alfred S. McEwen b, Joseph M. Boyce c, Veronica J. Bray b, Christy M. Caudill b, John A. Grant d, Christopher W. Hamilton e, Sarah Mattson b, Peter J. Mouginis-Mark c a University of Western Ontario, Centre for Planetary Science and Exploration, Earth Sciences, London, ON, Canada N6A 5B7 b University of Arizona, Lunar and Planetary Lab, Tucson, AZ 85721-0092, USA c University of Hawai’i, Hawai’i Institute of Geophysics and Planetology, Ma¯noa, HI 96822, USA d Smithsonian Institution, Center for Earth and Planetary Studies, Washington, DC 20013-7012, USA e NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA article info abstract Article history: Recently acquired high-resolution images of martian impact craters provide further evidence for the Received 28 August 2011 interaction between subsurface volatiles and the impact cratering process. A densely pitted crater-related Revised 29 April 2012 unit has been identified in images of 204 craters from the Mars Reconnaissance Orbiter. This sample of Accepted 9 May 2012 craters are nearly equally distributed between the two hemispheres, spanning from 53°Sto62°N latitude. Available online 24 May 2012 They range in diameter from 1 to 150 km, and are found at elevations between À5.5 to +5.2 km relative to the martian datum. The pits are polygonal to quasi-circular depressions that often occur in dense clus- Keywords: ters and range in size from 10 m to as large as 3 km. -
The New Engineering Research Centers: Purposes, Goals, and Expectations
DOCUMENT RESUME ED 315 272 SE 051 142 TITLE The New Engineering Research Centers: Purposes, Goals, and Expectations. Symposium (District of Colombia, April 29-30, 1985). INSTITUTION National Academy of Sciences - National Research Council, Washington, DC. Commission on Engineering and Technical Systems. SPONS AGENCY National Science Foundation, Washington, D. REPORT NO ISBN-0-309-03598-8 PUB DATE 86 GRANT NSF-MEG-8505051 NOTE 213p.; Prepared by the Cross-Disciplinary Engineering Research Committee. AVAILABLE FROM National Academy Press, 1201 Constitution Ave. N.W., Washington, DC 20418 ($25.95). PUB TYPE Collected Works - Conference Proceedings (021) -- Viewpoints (120) EDRS PRICE MF01 Plus Postage. PC Not Available from EDRS. DESCRIPTORS *Engineering; *Engineering Education; *Engineering Technology; *Research Administration; Research and Development; *Research and Development Centers; Research Directors; Research Proposals; Scientific Research IDENTIFIERS *Engineering Research Centers ABSTRACT The aympoisum was held to describe the roots and future plans of the Engineering Research Center's (ERC's) concept and program. The first section of this symposium compilation describes the national goals that the ERCs represent. The second section presents the point of view of the National Science Foundation on the ERCs--the concept behind them, their goals, selection criteria, and mechanisms for support. The next section provides the plans and programs of the six existing centers:(1) Systems Research Center; (2) Center for Intelligent Manufacturin3 Systems;(3) Center for Robotic Systems in Microelectronics; (4) Center for Composites Manufacturing Science and Engineering; (5) Engineering Center for Telecommunications; and (6) Biotechnology Process Engineering Center. Two of the presentations were on exchange methods among the centers and the relationship between engineering.education and research. -
2021-03 Pearcey Newby and the Vulcan V2.Pdf
Journal of Aeronautical History Paper 2021/03 Pearcey, Newby, and the Vulcan S C Liddle Vulcan to the Sky Trust ABSTRACT In 1955 flight testing of the prototype Avro Vulcan showed that the aircraft’s buffet boundary was unacceptably close to the design cruise condition. The Vulcan’s status as one of the two definitive carrier aircraft for Britain’s independent nuclear deterrent meant that a strong connection existed between the manufacturer and appropriate governmental research institutions, in this case the Royal Aircraft Establishment (RAE) and the National Physical Laboratory (NPL). A solution was rapidly implemented using an extended and drooped wing leading edge, designed and high-speed wind-tunnel tested by K W Newby of RAE, subsequently being fitted to the scaled test version of the Vulcan, the Avro 707A. Newby’s aerodynamic solution exploited a leading edge supersonic-expansion, isentropic compression* effect that was being investigated at the time by researchers at NPL, including H H Pearcey. The latter would come to be associated with this ‘peaky’ pressure distribution and would later credit the Vulcan implementation as a key validation of the concept, which would soon after be used to improve the cruise efficiency of early British jet transports such as the Trident, VC10, and BAC 1-11. In turn, these concepts were exploited further in the Hawker-Siddeley design for the A300B, ultimately the basis of Britain’s status as the centre of excellence for wing design in Airbus. Abbreviations BS Bristol Siddeley L Lift D Drag M Mach number CL Lift Coefficient NPL National Physical Laboratory Cp Pressure coefficient RAE Royal Aircraft Establishment Cp.te Pressure coefficient at trailing edge RAF Royal Air Force c Chord Re Reynolds number G Load factor t Thickness HS Hawker Siddeley WT Wind tunnel HP Handley Page α Angle of Attack When the airflow past an aerofoil accelerates its pressure and temperature drop, and vice versa. -
Martian Subsurface Properties and Crater Formation Processes Inferred from Fresh Impact Crater Geometries
Martian Subsurface Properties and Crater Formation Processes Inferred From Fresh Impact Crater Geometries The Harvard community has made this article openly available. Please share how this access benefits you. Your story matters Citation Stewart, Sarah T., and Gregory J. Valiant. 2006. Martian subsurface properties and crater formation processes inferred from fresh impact crater geometries. Meteoritics and Planetary Sciences 41: 1509-1537. Published Version http://meteoritics.org/ Citable link http://nrs.harvard.edu/urn-3:HUL.InstRepos:4727301 Terms of Use This article was downloaded from Harvard University’s DASH repository, and is made available under the terms and conditions applicable to Other Posted Material, as set forth at http:// nrs.harvard.edu/urn-3:HUL.InstRepos:dash.current.terms-of- use#LAA Meteoritics & Planetary Science 41, Nr 10, 1509–1537 (2006) Abstract available online at http://meteoritics.org Martian subsurface properties and crater formation processes inferred from fresh impact crater geometries Sarah T. STEWART* and Gregory J. VALIANT Department of Earth and Planetary Sciences, Harvard University, 20 Oxford Street, Cambridge, Massachusetts 02138, USA *Corresponding author. E-mail: [email protected] (Received 22 October 2005; revision accepted 30 June 2006) Abstract–The geometry of simple impact craters reflects the properties of the target materials, and the diverse range of fluidized morphologies observed in Martian ejecta blankets are controlled by the near-surface composition and the climate at the time of impact. Using the Mars Orbiter Laser Altimeter (MOLA) data set, quantitative information about the strength of the upper crust and the dynamics of Martian ejecta blankets may be derived from crater geometry measurements.