2021 Suzuki Hayabusa

Total Page:16

File Type:pdf, Size:1020Kb

2021 Suzuki Hayabusa 1999-2021 HAYABUSA 12-PAGE BUSA SPECIAL IS BACK! EXCLUSIVE IN-DEPTH ANALYSIS l Faster, lighter and sharper! + The evolution of a legend + NEW BUSA STRIPPED P6 2021 SUZUKI HAYABUSA NEW BIKE SPECIAL Return of the 1999-2021 ‘All everyone original wanted to know hyperbike HAYABUSA If you thought the hyperbike 12-PAGE was how fast it was’ class had finally gone the SPECIAL way of the dinosaurs – CELEBRATING 22 YEARS OF SUZUKI’S HAYABUSA think again. While Suzuki’s ground-breaking Hayabusa has been absent from our shores for a couple of years, it’s now returned just in time to have the sector to WELCOME Richard Newland, Editor itself. It’s lighter, faster, and bristling with new tech. We go under the skin of the new ‘I was flat-out Busa and also look back at 22 years of going ballistic. on the limiter at 186mph’ One of the moments I’ll never forget in my biking life was blasting down the 2-mile long straight at Bruntingthorpe Proving Ground on a Suzuki Hayabusa as it bumped into its limiter in 6th gear. I don’t know how fast I was really going, but it was somewhere north of 180mph. They were limited to 300kmh – that’s 186mph, for a less lardy pilot. What’s the relevance in the ‘real world’? Not a lot, really. Yes, you could go Autobahn baiting on your summer holidays if you have a death wish, or enjoy trying to eke the last few tenths out at somewhere like Elvington, but that momentary top-speed thrill isn’t the real joy of a bike like the Hayabusa. While I never really fell in love with the hyperbike hyperbole, I’ve always relished the extraordinary sensations you get from that exclusive club of rear-tyre-bothering behemoths. Whether it’s the Hayabusa, ZX-12R, H2 SX, ZZR1400, Blackbird... They all have a quality of drive that’s unmistakably different from the norm. So I’m delighted the Hayabusa is back from the wilderness; faster, lighter and sharper than ever. I can’t wait to see just how good it feels in 2021. 02 | Hayabusa Special 1999 - 2021 www.bikes.suzuki.co.uk www.bikes.suzuki.co.uk 1999 - 2021 Hayabusa Special | 03 2021 SUZUKI HAYABUSA Exclusive MCN Special The Busa 1999-2021 HAYABUSA 12-PAGE is back! SPECIAL Suzuki have breathed new life into the original horizon-shrinker – we speak exclusively to the engineers and designers who created the new Hayabusa he 200mph club MotoGP engines such as the 800cc comprised a short- HIGHLIGHTS V4 and 1000cc inline-four which lived explosion Joan Mir won the championship of speed-chasing l 1340cc l/c DOHC inline-four with. But I applied for the hyperbikes that l 187.74bhp @ 9700rpm Hayabusa development team as it hovered menacingly was the reason I joined Suzuki.” around the new l 110.6lb.ft @ 7000rpm Tmillennium like the ominous bug l 264kg kerb mass The same but better that threatened to erase every l The mantras that underpinned the computer on Earth. Of course, they 800mm seat height chassis and engine development couldn’t really do 200mph, but the l Price £16,499 also flowed through the design millennium bug wasn’t real either. language of the new Busa. As the anti-speed lobby girded “I faced lots of difficulties in its loins in preparation for a fight, parts therein – from the crankshaft designing the third-generation the Japanese initiated a self- to the valve train and everything Hayabusa; to keep the traditional policed 300kmh restriction to ‘It had to keep its silhouette, in between – are new. “The engine silhouette, but integrate new deflect more severe legislative development from Gen2 to Gen3, essence and tastes in it,” says meddling – and as soon as the wax despite keeping capacity the Kazutaka Ogawa, Styling Designer. started to solidify on the new pact, to be recognisably a Busa’ same, is actually greater than the “It had to be recognisably a new the game had already changed. changes from Gen1 (1298cc) to Hayabusa, not just any sportsbike. The Hayabusa still felt like Gen2 (1340cc),” says Shunya Togo, My first job at Suzuki was in the apex predator, snarling at superchargers, turbos, every pots. Neither were deemed more Engine Test Engineer. wind tunnel testing the first Honda’s oh-so-refined Blackbird rider aid known to Bosch and a balanced or effective than the Gen2 Balance is the key here. Suzuki’s generation Hayabusa, which gave and Kawasaki’s brutish ZX-12R special hoverboard switch, then engine and chassis package they obsessive total-package mentality me the knowledge to overcome the and ubiquitous ZZR11/12/14 – but you’re both missing the point and were trying to better. that saw them clinch the MotoGP difficulty of optimising the balance they all danced to a similar tune: staring into a (now LED) cyclops “There was an option to take crown in 2020 is now being driven between the comfort of the rider Big inline-four, acres of slippery eye of disappointment. Yes, it looks the Hayabusa in a new direction into their road bikes. As Chief and aerodynamics at 300kmh.” plastic, rider-cocooning capsules familiar. Yes, the engine capacity with a new engine,” says Naoki Engineer Fumihiro Onishi puts it: Suzuki say it’s taken them a ‘The new of aerodynamic efficiency – and is identical to the Gen2 model and Mizoguchi, Engine Designer. “But “The new Hayabusa has inherited decade of development to deliver a promise that the adage of ‘it’s a the twin-spar main frame remains while comparing prototypes with our Suzuki DNA, no compromise in this evolutionary step – something small world’ would feel even more unchanged, too. Yes, it’s lost a little the second-generation model engineering for ‘basic performance that is hard to accept without horizon-shrinkingly true onboard. peak power and torque – while we found that its engine offered as the basis of all’.” But why knowing what they tried during Hayabusa should pleasingly filling them in right better all-around performance. not adopt variable valve timing the process. “Our target was to The Emperor’s new clothes where you want it in the midrange. Therefore, we used the second- from the GSX-R1000? “The make the ultimate sport bike. And here we are, 22 years after If that’s the ‘less’, the ‘more’ is generation engine as a basis from new Hayabusa achieves target It took time to determine what be faster than its the first Hayabusa shocked us that it’s actually faster than its which to improve the power and performance without a variable equipment and price range were with its jelly-mould oddness and forebears and should be more torque in the low to mid-range.” valve mechanism.” required, and to achieve through blistering pace, looking at the agile too, thanks to a tidal surge of This transparency over aborted Without the need for a complex trial and error the performance, third generation of the species electronics and weight loss. development directions is unusual VVT system, servicing will be style and traditional Suzuki forebears and – a sole survivor of the class. from any manufacturer, let alone cheaper, reliability and durability durability that would meet and SUZUKI We could dismiss it by saying The power to move you a Japanese one, and underlines greater, and the overall cost of the exceed expectations,” says Kenichi it’s an evolution of Porsche 911 This isn’t the epitome of lazy their conviction that the new Busa bike constrained. And if you need Kasuya, Assistant Chief Engineer. PICTURES WATCH more agile, too’ proportions (ie: akin to a game of evolution, though. Suzuki’s is chasing the best solution, not more power for the strip, fit a non- “We have kept customers waiting ‘spot the difference’) – but that engineers built a turbo-charged marketing headlines. Euro5 exhaust: “If I am supposed – but are confident the new THE VIDEO would be an injustice. Not least version of the 1340cc second-gen The pursuit of mid-range torque to join a drag race, I will choose the Hayabusa will be worth the wait.” at motorcyclenews.com because of the journey Suzuki went engine to see if they could make is cited as another reason for siding new Hayabusa without hesitation,” on to find their way back home. forced induction work. Then they with capacity, rather than forced says Shunya Togo. He knows a bit RICHARD NEWLAND If you’re looking for pub- built an inline-six with a shade induction. While the capacity and about engine development, too: Let’s go under the skin... bragging power and torque figures, over 1000cc combined between its crankcases remain, the moving “I was engaged in development of WORDS 04 | Hayabusa Special 1999 - 2021 www.bikes.suzuki.co.uk www.bikes.suzuki.co.uk 1999 - 2021 Hayabusa Special | 05 2021 SUZUKI HAYABUSA Holding it Stopping The grunt factory 4 together 5 power 6 Suzuki used the 1340cc extraordinarily powerful performance.” 1999-2021 inline-four from the Gen2 Headline improvements include: Intake The Gen2 aluminium twin-spar Braking power is provided by Brembo Busa as their base, but it’s not the same and exhaust cams get revised profiles frame proved to be more balanced Stylema calipers mated to bigger engine, with major updates to essentially to reduce overlap, valve spring load is Under the skin than any new variations they tested 320mm discs, assisted by the latest every component other than the increased to cope with the increased lift, HAYABUSA during development, so it remains cornering ABS and a combined crankcases.
Recommended publications
  • 2018 RULEBOOK PRO STREET Changes from Last Season Are Made in BLUE
    2018 RULEBOOK PRO STREET Changes from last season are made in BLUE. Revisions during the season are made in RED. Revised 3/7/18 CLASS DESCRIPTION: This class contests the ultimate in street‐legal motorcycles. Created to legitimize illicit street racing, Pro Street is reserved for stock‐appearing motorcycles with unlimited engine modifications. All bikes must be street legal and be powered by self‐starting motorcycle engines. DESIGNATION: The class designation is PST. All entrants must display this designation on both sides of their motorcycle by their bike number. FORMAT: This is a 1/4 mile heads‐up class run on a .400 pro tree. The class will qualify a 16‐bike field and place them on a pro ladder. There will also be a "B Class” for riders that qualified 17th – 32nd and they will be placed on a separate pro ladder. No alternates will be used in either class if a rider is broken. CHANGING BIKES: A racer can change his or her bike in qualifying if there is still another qualifying session for the class, however all previous qualifying data will be erased and the racer must re‐qualify the new bike (You still need to notify the tower to change). The bike and rider that runs first round is the one that must be used for the remainder of eliminations, even if the class is completed on another weekend due to weather. POINTS: This class will be a points class at all XDA, MAN CUP & NHDRO events. BIG‐BORE BIKES: Production big‐bore bikes are permitted a single power adder.
    [Show full text]
  • How a Cartoon Series Helped the Public Care About Rosetta and Philae 13 How a Cartoon Series Helped the Public Care About Rosetta and Philae
    How a Cartoon Series Helped the Public Care about Best Practice Rosetta and Philae Claudia Mignone Anne-Mareike Homfeld Sebastian Marcu Vitrociset Belgium for European Space ATG Europe for European Space Design & Data GmbH Agency (ESA) Agency (ESA) [email protected] [email protected] [email protected] Carlo Palazzari Emily Baldwin Markus Bauer Design & Data GmbH EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) [email protected] [email protected] [email protected] Keywords Karen S. O’Flaherty Mark McCaughrean Outreach, space science, public engagement, EJR-Quartz for European Space Agency (ESA) European Space Agency (ESA) visual storytelling, fairy-tale, cartoon, animation, [email protected] [email protected] anthropomorphising Once upon a time... is a series of short cartoons1 that have been developed as part of the European Space Agency’s communication campaign to raise awareness about the Rosetta mission. The series features two anthropomorphic characters depicting the Rosetta orbiter and Philae lander, introducing the mission story, goals and milestones with a fairy- tale flair. This article explores the development of the cartoon series and the level of engagement it generated, as well as presenting various issues that were encountered using this approach. We also examine how different audiences responded to our decision to anthropomorphise the spacecraft. Introduction internet before the spacecraft came out of exciting highlights to come, using the fairy- hibernation (Bauer et al., 2016). The four tale narrative as a base. The hope was that In late 2013, the European Space Agency’s short videos were commissioned from the video would help to build a degree of (ESA) team of science communicators the cross-media company Design & Data human empathy between the public and devised a number of outreach activ- GmbH (D&D).
    [Show full text]
  • Science Exploration and Instrumentation of the OKEANOS Mission to a Jupiter Trojan Asteroid Using the Solar Power Sail
    Planetary and Space Science xxx (2018) 1–8 Contents lists available at ScienceDirect Planetary and Space Science journal homepage: www.elsevier.com/locate/pss Science exploration and instrumentation of the OKEANOS mission to a Jupiter Trojan asteroid using the solar power sail Tatsuaki Okada a,b,*, Yoko Kebukawa c,d, Jun Aoki d, Jun Matsumoto a, Hajime Yano a, Takahiro Iwata a, Osamu Mori a, Jean-Pierre Bibring e, Stephan Ulamec f, Ralf Jaumann g, Solar Power Sail Science Teama a Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, 252-5210, Japan b The University of Tokyo, Hongo, Bunkyo, Tokyo, Japan c Faculty of Engineering, Yokohama National University, Japan d Graduate School of Science, Osaka University, Toyonaka, Japan e Institut dʼAstrophysique Spatiale, Orsay, France f German Aerospace Center, Cologne, Germany g German Aerospace Center, Berlin, Germany ARTICLE INFO ABSTRACT Keywords: An engineering mission OKEANOS to explore a Jupiter Trojan asteroid, using a Solar Power Sail is currently under Solar system formation study. After a decade-long cruise, it will rendezvous with the target asteroid, conduct global mapping of the Jupiter trojans asteroid from the spacecraft, and in situ measurements on the surface, using a lander. Science goals and enabling Solar power sail instruments of the mission are introduced, as the results of the joint study between the scientists and engineers Lander from Japan and Europe. Mass spectrometry OKEANOS 1. Introduction ocean water and life. Lucy (Levison et al., 2017), a Jupiter Trojan multi-flyby mission, has Jupiter Trojan asteroids are located in the long-term stable orbits been selected as a NASA Discovery class mission, which aims for un- around the Sun-Jupiter Lagrange points (L4 or L5) Most of them are derstanding the variation and diversity of Jupiter Trojans.
    [Show full text]
  • Planet Earth Taken by Hayabusa-2
    Space Science in JAXA Planet Earth May 15, 2017 taken by Hayabusa-2 Saku Tsuneta, PhD JAXA Vice President Director General, Institute of Space and Astronautical Science 2017 IAA Planetary Defense Conference, May 15-19,1 Tokyo 1 Brief Introduction of Space Science in JAXA Introduction of ISAS and JAXA • As a national center of space science & engineering research, ISAS carries out development and in-orbit operation of space science missions with other directorates of JAXA. • ISAS is an integral part of JAXA, and has close collaboration with other directorates such as Research and Development and Human Spaceflight Technology Directorates. • As an inter-university research institute, these activities are intimately carried out with universities and research institutes inside and outside Japan. ISAS always seeks for international collaboration. • Space science missions are proposed by researchers, and incubated by ISAS. ISAS plays a strategic role for mission selection primarily based on the bottom-up process, considering strategy of JAXA and national space policy. 3 JAXA recent science missions HAYABUSA 2003-2010 AKARI(ASTRO-F)2006-2011 KAGUYA(SELENE)2007-2009 Asteroid Explorer Infrared Astronomy Lunar Exploration IKAROS 2010 HAYABUSA2 2014-2020 M-V Rocket Asteroid Explorer Solar Sail SUZAKU(ASTRO-E2)2005- AKATSUKI 2010- X-Ray Astronomy Venus Meteorogy ARASE 2016- HINODE(SOLAR-B)2006- Van Allen belt Solar Observation Hisaki 2013 4 Planetary atmosphere Close ties between space science and space technology Space Technology Divisions Space
    [Show full text]
  • Science Instruments on Hayabusa Follow-On Missions
    Science Instruments on Hayabusa follow-on missions Yasuhiko Takagi (Aichi Toho University) (prepared by Masanao Abe (JAXA)) 1 Science instruments under examination Others 2 Basic concept of Hayabusa-IF* camera • Use Navigation camera as a scientific imager • Similar optics and CCD as AMICA, but with minor modifications on – Filters • ECAS -> special set for C-type • Remove ND flter , polarizer on CCD – Electronics • More flexible and autonomous operation • More effective compression • Larger onboard storage • Onboard data analysis 3 *Hayabusa-IF: Hayabusa Immediate Follow-on mission AMICA on Hayabysa Polarizer 4 Ground-based ECAS Quasi ECAS filters on AMICA5 A new filter set • Narrower band width (5~20 nm) – Remove ND filter – More accurate colorimetry • UV absorption as a thermal metamorphism indicator? • Phyllosilicate absorption around 700nm (430nm ?) • Nearby reference bands • Wide filter for imaging stars and the artificial orbiters (~TM) • Natural RGB for outreach purpose? • Several common bands with previous missions? (SSI/Galileo, MSI/NEAR, AMICA/Hayabusa, FC/ Dawn, NAC/Stardust, ??/Rosetta,etc, ) 6 Ground-based ECAS Thermal alteration Phyllosilicate absorption 7 8 Hayabusa NIRS • Wavelength range: 764-2247nm (△λ23.56nm) • FOV: 0.1x0.1deg(9m@5km distance) • Detector: InGaAs Liner Array (64channels) • F value: 1.00 • Effective diameter: 27mm • Operating temperature: 260K • A/D resolution (dynamic range) : 14bits 1 Average 0.1 Output [V] [V] Output Output 0.01 Standard Deviation 0.001 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 2.2 2.4 9 Wavelength
    [Show full text]
  • Overcoming the Challenges Associated with Image-Based Mapping of Small Bodies in Preparation for the OSIRIS-Rex Mission to (101955) Bennu
    Preprint of manuscript submitted to Earth and Space Science Overcoming the Challenges Associated with Image-based Mapping of Small Bodies in Preparation for the OSIRIS-REx Mission to (101955) Bennu D. N. DellaGiustina1, C. A. Bennett1, K. Becker1, D. R Golish1, L. Le Corre2, D. A. Cook3†, K. L. Edmundson3, M. Chojnacki1, S. S. Sutton1, M. P. Milazzo3, B. Carcich4, M. C. Nolan1, N. Habib1, K. N. Burke1, T. Becker1, P. H. Smith1, K. J. Walsh5, K. Getzandanner6, D. R. Wibben4, J. M. Leonard4, M. M. Westermann1, A. T. Polit1, J. N. Kidd Jr.1, C. W. Hergenrother1, W. V. Boynton1, J. Backer3, S. Sides3, J. Mapel3, K. Berry3, H. Roper1, C. Drouet d’Aubigny1, B. Rizk1, M. K. Crombie7, E. K. Kinney-Spano8, J. de León9, 10, J. L. Rizos9, 10, J. Licandro9, 10, H. C. Campins11, B. E. Clark12, H. L. Enos1, and D. S. Lauretta1 1Lunar and Planetary Laboratory, University of Arizona, Tucson, AZ, USA 2Planetary Science Institute, Tucson, AZ, USA 3U.S. Geological Survey Astrogeology Science Center, Flagstaff, AZ, USA 4KinetX Space Navigation & Flight Dynamics Practice, Simi Valley, CA, USA 5Southwest Research Institute, Boulder, CO, USA 6Goddard Spaceflight Center, Greenbelt, MD, USA 7Indigo Information Services LLC, Tucson, AZ, USA 8 MDA Systems, Ltd, Richmond, BC, Canada 9Instituto de Astrofísica de Canarias, Santa Cruz de Tenerife, Spain 10Departamento de Astrofísica, Universidad de La Laguna, Santa Cruz de Tenerife, Spain 11Department of Physics, University of Central Florida, Orlando, FL, USA 12Department of Physics and Astronomy, Ithaca College, Ithaca, NY, USA †Retired from this institution Corresponding author: Daniella N.
    [Show full text]
  • Asteroid Explorer, Hayabusa2, Reporter Briefing
    Asteroid explorer, Hayabusa2, reporter briefing November 30, 2020 JAXA Hayabusa2 Project Topics Regarding Hayabusa2 Results from TCM-3 Details of capsule separation and re-entry Preparation status for capsule collection 2020/11/30 Hayabusa2 reporter briefing 2 Contents 0. Hayabusa2 and mission flow outline 1. Current status and overall schedule of the project 2. Results from TCM-3 3. Details of capsule separation and re-entry 4. Preparation status for capsule collection 5. Outreach 6. Future plans 2020/11/30 Hayabusa2 reporter briefing 3 Overview of Hayabusa2 Objective We will explore and sample the C-type asteroid Ryugu, which is a more primitive type than the S-type asteroid Itokawa that Hayabusa explored, and elucidate interactions between minerals, water, and organic matter in the primitive solar system. By doing so, we will learn about the origin and evolution of Earth, the oceans, and life, and maintain and develop the technologies for deep-space return exploration (as demonstrated with Hayabusa), a field in which Japan leads the world. Expected results and effects By exploring a C-type asteroid, which is rich in water and organic materials, we will clarify interactions between the building blocks of Earth and the evolution of its oceans and life, thereby developing solar system science. Japan will further its worldwide lead in this field by taking on the new challenge of obtaining samples from a crater produced by an impacting device. We will establish stable technologies for return exploration of solar-system bodies. Features: (Illustration: Akihiro Ikeshita) World’s first sample return mission to a C-type asteroid.
    [Show full text]
  • Dr. Chit Hong Yam Japan Aerospace Exploration Agency (JAXA), ISAS, Japan, [email protected]
    Paper ID: 25610 65th International Astronautical Congress 2014 oral ASTRODYNAMICS SYMPOSIUM (C1) Mission Design, Operations and Optimization (2) (9) Author: Dr. Chit Hong Yam Japan Aerospace Exploration Agency (JAXA), ISAS, Japan, [email protected] Dr. Yoshihide Sugimoto Japan Aerospace Exploration Agency (JAXA), ISAS, Japan, [email protected] Mr. Naoya Ozaki University of Tokyo, Japan, [email protected] Mr. Bruno Sarli The Graduate University for Advanced Studies (Sokendai), Japan, [email protected] Ms. Hongru Chen Kyushu University, Japan, [email protected] Dr. Stefano Campagnola Japan Aerospace Exploration Agency (JAXA), Japan, [email protected] Mr. Satoshi Ogura The University of TOKYO, Graduate school, Japan, [email protected] Mr. Yosuke Kawabata Japan Aerospace Exploration Agency (JAXA), ISAS, Japan, [email protected] Dr. Yasuhiro Kawakatsu Japan Aerospace Exploration Agency (JAXA), Japan, [email protected] Mr. shintaro nakajima University of Tokyo, Japan, [email protected] Prof. Ryu Funase University of Tokyo, Japan, [email protected] Prof. Shinichi Nakasuka University of Tokyo, Japan, [email protected] LAUNCH WINDOW AND SENSITIVITY ANALYSIS OF AN ASTEROID FLYBY MISSION WITH MINIATURE ION PROPULSION SYSTEM: PROCYON Abstract PROCYON (PRoximate Object Close flYby with Optical Navigation) is a mission aimed to demon- strate the technology of a micro spacecraft deep space exploration and proximity flyby to asteroids. The mission is developed by the University of Tokyo in collaboration with JAXA. The spacecraft is scheduled to be launched as a secondary payload in December 2014 with Hayabusa 2 spacecraft.
    [Show full text]
  • ISAS's Deep Space Fleet Electric Propulsion Expands Horizon of Human Activities
    ISAS’s Deep Space Fleet Electric Propulsion Expands Horizon of Human Activities IEPC-2019-939 Presented at the 36th International Electric Propulsion Conference University of Vienna • Vienna, Austria September 15-20, 2019 Hitoshi Kuninaka Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Yoshinodai, Chuo, Sagamihara, Kanagawa 252-5210 JAPAN Abstract: Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency is now putting our space assets from Mercury to Jupiter, and then will accomplish to make the ISAS’s Deep Space Fleet in the Solar System. After the powered flight in 3.5 years by the microwave discharge ion engines, Hayabusa2 is exploring asteroid Ryugu in 2019. ESA’s BepiColombo with ISAS’s Mio is going to Mercury by T6 ion engines. DESTINY+ will flyby asteroid Phaethon using the microwave discharge ion engines. Akatsuki is circulating around Venus. SLIM is under development to land on Moon. MMX will achieve the sample return from Phobos of Mars. ISAS cooperates with ESA in JUICE mission toward Jupiter. In the ISAS’s Deep Space Fleet the electric propulsion plays an important role. I. Introduction nstitute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA) is now putting Iour space assets from Mercury to Jupiter, and then will accomplish to make the ISAS’s Deep Space Fleet in space, illustrated in Fig.1, in which a lot of spacecraft swarm to investigate the history of the solar system in 4.7 billion years. Akatsuki is an active Venus probe. SLIM is under development for a lunar lander. MMX aims to the sample return from Phobos of Mars.
    [Show full text]
  • The Near Earth Object (NEO) Scout Spacecraft: a Low-Cost Approach to In-Situ Characterization of the NEO Population
    The Near Earth Object (NEO) Scout Spacecraft: A low-cost approach to in-situ characterization of the NEO population Eric A. Woeppel,1 James M. Balsamo,1 Karl J. Fischer,1 Matthew J. East,1 Jeremy A. Styborski,1 Christopher A. Roche,1 Mackenzie D. Ott,1 Matthew J. Scorza,1 Christopher D. Doherty, 1 Andrew J. Trovato,1 and Christopher P. Volk1 Rensselaer Polytechnic Institute, Troy, NY, 12180, USA Dr. Steven L. Koontz2 NASA JSC, Houston, TX, 77058, USA Dr. Riccardo Bevilacqua3 Rensselaer Polytechnic Institute, Troy, NY, 12180, USA Dr. Charles Swenson4 Utah State University, Logan, Utah 84322-1400, USA This paper describes a microsatellite spacecraft with supporting mission profile and architecture, designed to enable preliminary in-situ characterization of a significant number of Near Earth Objects (NEOs) at reasonably low cost. The spacecraft will be referred to as the NEO- Scout. NEO-Scout spacecraft are to be placed in Geosynchronous Equatorial Orbit (GEO), cis- lunar space, or on earth escape trajectories as secondary payloads on launch vehicles headed for GEO or beyond, and will begin their mission after deployment from the launcher. A distinguishing key feature of the NEO-Scout system is to design the spacecraft and mission timeline so as to enable rendezvous with and landing on the target NEO during NEO close approach (<0.3 AU) to the Earth-Moon system using low-thrust/high-impulse propulsion systems. Mission durations are on the order 100 to 400 days. Mission feasibility and preliminary design analysis are presented, along with
    [Show full text]
  • The MASCOT Camera on Hayabusa-2'S Asteroid Lander
    46th Lunar and Planetary Science Conference (2015) 1799.pdf The MASCOT Camera on Hayabusa-2’s asteroid lander MASCOT (Mobile Asteroid Surface Scout). N. Schmitz1, A. Koncz1, R. Jaumann1, H. Hoffmann1, D. Jobs1, J. Kachlicki1, H. Michaelis1, S. Mottola1, B. Pforte1, S. Schroeder1, R. Terzer1, F. Trauthan1, M. Tschentscher1, S. Weisse1, T.-M. Ho2, J. Biele3, S. Ulamec3, B. Broll4, A. Kruselburger4, L. Perez-Prieto4. 1DLR, Institute of Planetary Research, Berlin, Germany, [email protected], 2DLR, Institute of Space Systems, Bremen, Germany, 3DLR-MUSC, Linder Höhe, Cologne, Germany, 4Airbus DS, Germany. Introduction: The MASCOT Camera (MSC sun angles over the course of a day will also contribute CAM) is part of the MASCOT lander’s science pay- to the physical characterization of the asteroid surface load. The MASCOT lander (Mobile Asteroid Surface by allowing to characterize time-dependent processes Scout) has been launched to asteroid 1999JU3 onboard and the photometric properties of the regolith. The JAXA’s Hayabusa-2 asteroid sample return mission on MASCOT camera observations, combined with the Dec 3rd, 2014. It is scheduled to arrive at 1999JU3 in MASCOT hyperspectral microscope and radiometer 2018, and return samples to Earth by 2020. spectral observations, will cover a wide range of ob- servational scales and serve as a strong tie point be- tween Hayabusa-2’s remote sensing science (103 -10- 3m) and sample science (10-3 -10-6 m). [3,4] Material properties Collaborating instruments Space Weathering NIRS3 Physical Properties Termal NIRS3, TIR Metamorphism Intra-grain texture SMP Anhydrous Minerals MSC Grain properties size, shape size, SMP strength porosity, NIRS3, LIDAR SCI experimentCrater SMP Organics TIR Natural craters SCI t50$ Figure 1.
    [Show full text]
  • Why Space Flight? the National Aeronautics and Space Act (1958)
    NASA and Future Human Exploration of the Solar System Presentation to the Westinghouse Science Honors Institute Monroeville, PA Bryan Palaszewski NASA Glenn Research Center Cleveland, OH October 17, 2015 Introduction • Why space flight? • The Space Act and Technology Development. • Human exploration of space (in the past). • Transitions. • New Space Launch System. • Robotic Mars Exploration. • Pluto and New Horizons. • Concluding remarks. Why Space Flight? The National Aeronautics and Space Act (1958) • (1) The expansion of human knowledge of the Earth and of phenomena in the atmosphere and space; • (2) The improvement of the usefulness, performance, speed, safety, and efficiency of aeronautical and space vehicles; • (3) The development and operation of vehicles capable of carrying instruments, equipment, supplies, and living organisms through space; • (4) The establishment of long-range studies of the potential benefits to be gained from, the opportunities for, and the problems involved in the utilization of aeronautical and space activities for peaceful and scientific purposes; • (5) The preservation of the role of the United States as a leader in aeronautical and space science and technology and in the application thereof to the conduct of peaceful activities within and outside the atmosphere; Why Space Flight? The National Aeronautics and Space Act (1958) • (6) The making available to agencies directly concerned with national defense of discoveries that have military value or significance, and the furnishing by such agencies, to the
    [Show full text]