Modernizing the Launch Sector
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Cape Canaveral Air Force Station Support to Commercial Space Launch
The Space Congress® Proceedings 2019 (46th) Light the Fire Jun 4th, 3:30 PM Cape Canaveral Air Force Station Support to Commercial Space Launch Thomas Ste. Marie Vice Commander, 45th Space Wing Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ste. Marie, Thomas, "Cape Canaveral Air Force Station Support to Commercial Space Launch" (2019). The Space Congress® Proceedings. 31. https://commons.erau.edu/space-congress-proceedings/proceedings-2019-46th/presentations/31 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Cape Canaveral Air Force Station Support to Commercial Space Launch Colonel Thomas Ste. Marie Vice Commander, 45th Space Wing CCAFS Launch Customers: 2013 Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; Blue text – in work; * – sub-orbital CCAFS Launch Customers: 2013 Complex 39B: NASA SLS Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy NASA Space Launch System Launch Complex 39B February 4, 2013 Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; -
Douglas Missile & Space Systems Division
·, THE THOR HISTORY. MAY 1963 DOUGLAS REPORT SM-41860 APPROVED BY: W.H.. HOOPER CHIEF, THOR SYSTEMS ENGINEERING AEROSPACE SYSTEMS ENGINEERING DOUGLAS MISSILE & SPACE SYSTEMS DIVISION ABSTRACT This history is intended as a quick orientation source and as n ready-reference for review of the Thor and its sys tems. The report briefly states the development of Thor, sur'lli-:arizes and chronicles Thor missile and booster launch inGs, provides illustrations and descriptions of the vehicle systcn1s, relates their genealogy, explains sane of the per fon:iance capabilities of the Thor and Thor-based vehicles used, and focuses attention to the exploration of space by Douelas Aircraf't Company, Inc. (DAC). iii PREFACE The purpose of The Thor History is to survey the launch record of the Thor Weapon, Special Weapon, and Space Systems; give a systematic account of the major events; and review Thor's participation in the military and space programs of this nation. The period covered is from December 27, 1955, the date of the first contract award, through May, 1963. V �LE OF CONTENTS Page Contract'Award . • • • • • • • • • • • • • • • • • • • • • • • • • 1 Background • • • • • • • • • • • • • • • • • • • • • • • • • • • • l Basic Or�anization and Objectives • • • • • • • • • • • • • • • • 1 Basic Developmenta� Philosophy . • • • • • • • • • • • • • • • • • 2 Early Research and Development Launches • • • ·• • • • • • • • • • 4 Transition to ICBM with Space Capabilities--Multi-Stage Vehicles . 6 Initial Lunar and Space Probes ••••••• • • • • • • • -
European Space Surveillance and Tracking
2ndEuropean EU SST Webinar: Space Operations in Space Surveillance and Tracking 16Surveillance November 2020 –and14h CETTracking The EU SST activities received funding from the European Union programmes, notably from the Horizon 2020 research and innovation programme under grant agreements No 760459, No 785257, No 713630, No 713762 and No 634943, and the Copernicus and Galileo programme under grant agreements No 299/G/GRO/COPE/19/11109, No 237/GRO/COPE/16/8935 and No 203/G/GRO/COPE/15/7987. This Portal reflects only the SST Cooperation’s actions and the European Commission and the Research Executive Agency are not responsible for any use that may be made of the information it contains. 2nd EU SST Webinar Operations in Space Surveillance and Tracking Speakers Pascal María Antonia Cristina Florian João FAUCHER (CNES) RAMOS (CDTI) PÉREZ (CDTI) DELMAS (CNES) ALVES (EU SatCen) Pier Luigi Lt. Moreno Juan Christophe Rodolphe RIGHETTI PERONI (IT MoD) ESCALANTE MORAND (EEAS) MUÑOZ (EUMETSAT) (EC – DG ECHO) (EC-DG DEFIS) 2nd EU SST Webinar: Operations in Space Surveillance and Tracking 16 November 2020 3 Agenda (1/2) 14h00-14h10: Welcome to the 2nd EU SST Webinar [Moderator: Mr Oliver Rajan (EU SatCen)] 14h10-14h50: SST Support Framework: Safeguarding European space infrastructure • Overview, governance model, security relevance and future perspectives [SST Cooperation Chair: Dr Pascal Faucher (CNES)] EU SST Architecture & Service Provision Model • Sensors network • Database and Catalogue precursor • Services [Chair of the SST Technical Committee: -
액체로켓 메탄엔진 개발동향 및 시사점 Development Trends of Liquid
Journal of the Korean Society of Propulsion Engineers Vol. 25, No. 2, pp. 119-143, 2021 119 Technical Paper DOI: https://doi.org/10.6108/KSPE.2021.25.2.119 액체로켓 메탄엔진 개발동향 및 시사점 임병직 a, * ㆍ 김철웅 a⋅ 이금오 a ㆍ 이기주 a ㆍ 박재성 a ㆍ 안규복 b ㆍ 남궁혁준 c ㆍ 윤영빈 d Development Trends of Liquid Methane Rocket Engine and Implications Byoungjik Lim a, * ㆍ Cheulwoong Kim a⋅ Keum-Oh Lee a ㆍ Keejoo Lee a ㆍ Jaesung Park a ㆍ Kyubok Ahn b ㆍ Hyuck-Joon Namkoung c ㆍ Youngbin Yoon d a Future Launcher R&D Program Office, Korea Aerospace Research Institute, Korea b School of Mechanical Engineering, Chungbuk National University, Korea c Guided Munitions Team, Hyundai Rotem, Korea d Department of Aerospace Engineering, Seoul National University, Korea * Corresponding author. E-mail: [email protected] ABSTRACT Selecting liquid methane as fuel is a prevailing trend for recent rocket engine developments around the world, triggered by its affordability, reusability, storability for deep space exploration, and prospect for in-situ resource utilization. Given years of time required for acquiring a new rocket engine, a national-level R&D program to develop a methane engine is highly desirable at the earliest opportunity in order to catch up with this worldwide trend towards reusing launch vehicles for competitiveness and mission flexibility. In light of the monumental cost associated with development, fabrication, and testing of a booster stage engine, it is strategically a prudent choice to start with a low-thrust engine and build up space application cases. -
ESPA Ring Datasheet
PAYLOAD ADAPTERS | ESPA ESPA THE EVOLVED SECONDARY PAYLOAD ADAPTER ESPA mounts to the standard NSSL (formerly EELV) interface bolt pattern (Atlas V, Falcon 9, Delta IV, OmegA, Vulcan, Courtesy of Lockheed Martin New Glenn) and is a drop-in component in the launch stack. Small payloads mount to ESPA ports featuring either a Ø15-inch bolt circle with 24 fasteners or a 4-point mount with pads at each corner of a 15-inch square; both of these interfaces have become small satellite standards. ESPA is qualified to carry 567 lbs (257 kg), and a Heavy interface Courtesy of NASA (with Ø5/16” fastener hardware) has been introduced with a capacity of 991 lbs (450 kg). All small satellite mass capabilities require the center of gravity (CG) to be within 20 inches (50.8 cm) of the ESPA port surface. Alternative configurations can be accommodated. ESPA GRANDE ESPA Grande is a more capable version of ESPA with Ø24-inch ports; the ring height is typically 42 inches. The Ø24-inch port has been qualified by test to Courtesy of ORBCOMM & Sierra Nevada Corp. carry small satellites up to 1543 lb (700 kg). ESPA ESPA IS ADAPTABLE TO UNIQUE MISSION REQUIREMENTS • The Air Force’s STP-1 mission delivered multiple small satellites on an Atlas V. • NASA’s Lunar Crater Observation and Sensing Satellite (LCROSS): ESPA was the spacecraft hub for the LCROSS shepherding satellite in 2009. • ORBCOMM Generation 2 (OG2) launched stacks of two and three ESPA Grandes on two different Falcon 9 missions and in total deployed 17 satellites. -
Orbital Fueling Architectures Leveraging Commercial Launch Vehicles for More Affordable Human Exploration
ORBITAL FUELING ARCHITECTURES LEVERAGING COMMERCIAL LAUNCH VEHICLES FOR MORE AFFORDABLE HUMAN EXPLORATION by DANIEL J TIFFIN Submitted in partial fulfillment of the requirements for the degree of: Master of Science Department of Mechanical and Aerospace Engineering CASE WESTERN RESERVE UNIVERSITY January, 2020 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis of DANIEL JOSEPH TIFFIN Candidate for the degree of Master of Science*. Committee Chair Paul Barnhart, PhD Committee Member Sunniva Collins, PhD Committee Member Yasuhiro Kamotani, PhD Date of Defense 21 November, 2019 *We also certify that written approval has been obtained for any proprietary material contained therein. 2 Table of Contents List of Tables................................................................................................................... 5 List of Figures ................................................................................................................. 6 List of Abbreviations ....................................................................................................... 8 1. Introduction and Background.................................................................................. 14 1.1 Human Exploration Campaigns ....................................................................... 21 1.1.1. Previous Mars Architectures ..................................................................... 21 1.1.2. Latest Mars Architecture ......................................................................... -
Askeri Lojistikte Uzay Çağı Başlıyor Mu?
Askeri Lojistikte Uzay Çağı Başlıyor mu? zay alanında 60 yıldan fazla zamandır süren insan faaliyetleri, dünyadaki yaşam kalitesini artıran toplumsal faydalar üretti. Uzay araştırmalarının zorlukları, yeni bilimsel ve teknolojik bilgileri ateşleyerek, inovasyonun temel kaynaklarından biri oldu. Uzay araştırmaları, malzeme, enerji üretimi Uve enerji depolama, geri dönüşüm ve atık yönetimi, gelişmiş robotik, tıp ve medikal teknolojiler, ulaşım, mühendislik, bilgi işlem ve yazılım gibi alanlarda dünyaya anında fayda sağladı ve sağlamaya devam edecek. Bu alanlardan biri de roket teknolojisi… Uzay ekonomisinin lokomotifi olan fırlatma sektöründe son yıllarda büyük bir değişim yaşanıyor. Yerden fırlatmalı katı yakıtlı roketlerin maliyetini azaltma arayışları, yeniden kullanılabilir fırlatıcı sistemlerinin geliştirilmesine kapı araladı. Özel uzay şirketlerinin geliştirdiği yeniden kullanılabilir roketler, uzay çalışmalarının maliyetlerini azaltıp daha fazla oyuncunun uzayın olanaklarından yararlanmasının önünü açıyor. Yakın gelecekte yeniden kullanılabilir roketler yeryüzünde de bir ulaşım aracı hâline gelebilir. Örneğin ABD Hava Kuvvetleri, bu roketleri çatışma alanlarına veya insani yardım ihtiyacı duyulan bölgelere lojistik destek sağlamakta kullanmak için harekete geçti. ABD Uzay Kuvvetleri ile birlikte yürütülen Roket Kargo (Rocket Cargo) projesi1, geleneksel askeri kargo uçakları ile saatler hatta günler alabilecek 30 ila 100 ton arasındaki sevkiyatları yeniden kullanılabilir roketlerle 90 dakika2 içinde Dünya’nın herhangi bir noktasına -
Downloads/NASA SBIR Amp STTR Program Homepage - Fuel Cells and Electrolyzers for Space Applications - 2013-10-31.Pdf 10
Humanity and Space Retrieval of Near Earth Asteroids and Mining Technology An Interactive Qualifying Project submitted to the faculty of Worcester Polytechnic Institute In partial fulfillment of the requirement for Degree of Bachelor Science By Colin Cooper Project Advisor: Mayer Humi Abstract: The current cost to transport materials into space is approximated at $10,000 dollars per kilogram. Mass of payloads for human oriented space mission can be greatly decreased through obtaining resources in space. Water, being abundant on carbonaceous chondrite (C-type) asteroids, could provide radiation shielding, life support, and potential fuel. Resources could save NASA up to $10 billion annually for future manned missions, and be the starting point for a space highway. 2 Table of Contents: 1. Executive Summary. 4 2. Introduction . 5 3. Carbonaceous Chondrite Asteroids. 6 3.1 C-type Asteroids . 6 3.2 Fuel . 6 3.3 Hydrogen Fuel Cells . 10 3.4 Life Support . 10 3.5 Radiation Shielding . 11 4. Asteroid Candidates . 14 5. Mass Breakdown . 18 6. Launch Vehicle. 24 7. Orbital Mechanics . 25 8. Optical Mining. 28 9. Mechanical Design . 31 10. Final Considerations . 33 11. Conclusion . 37 12. Appendix . 39 13. References . … . 42 3 1. Executive Summary Humanity benefits from the advancement in technology made in the space industry. Technology created for use in space is often found to have applicable uses on Earth. More importantly, the ultimate goal of space exploration is the preservation of life on Earth. To do so, colonization is the only option. Asteroid mining technology will provide a necessary framework for future attempts at colonizing a planet. -
Space Coast Is Getting Busy: 6 New Rockets Coming to Cape Canaveral, KSC
4/16/2019 Space Coast is getting busy: 6 new rockets coming to Cape Canaveral, KSC Space Coast is getting busy: 6 new rockets coming to Cape Canaveral, Kennedy Space Center Emre Kelly, Florida Today Published 4:04 p.m. ET April 11, 2019 | Updated 7:53 a.m. ET April 12, 2019 COLORADO SPRINGS, Colo. – If schedules hold, the Space Coast will live up to its name over the next two years as a half-dozen new rockets target launches from sites peppered across the Eastern Range. Company, government and military officials here at the 35th Space Symposium, an annual space conference, have reaffirmed their plans to launch rockets ranging from more traditional heavy-lift behemoths to smaller vehicles that take advantage of new manufacturing technologies. Even if some of these schedules slip, at least one thing is apparent to several spaceflight experts here: The Eastern Range is seeing an unprecedented growth in commercial space companies and efforts. Space Launch System: 2020 NASA's Space Launch System rocket launches from Kennedy Space Center's pad 39B in this rendering by the agency. (Photo: NASA) NASA's long-awaited SLS, a multibillion-dollar rocket announced in 2011, is slated to become the most powerful launch vehicle in history if it can meet a stringent late 2020 deadline. The 322-foot-tall rocket is expected to launch on its first flight – Exploration Mission 1 – from Kennedy Space Center with an uncrewed Orion capsule for a mission around the moon, which fits in with the agency's wider goal of putting humans on the surface by 2024. -
Reusable Stage Concepts Design Tool
DOI: 10.13009/EUCASS2019-421 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Reusable stage concepts design tool Lars Pepermans?, Barry Zandbergeny ?Delft University of Technology Kluyverweg 1, 2629 HS Delft [email protected] yDelft University of Technology Kluyverweg 1, 2629 HS Delft Abstract Reusable launch vehicles hold the promise of substantially reducing the cost of access to space. Many different approaches towards realising a reusable rocket exist or are being proposed. This work focuses on the use of an optimisation method for conceptual design of non-winged reusable upper stages, thereby allowing it to take into account landing on land, sea or mid-air retrieval as well as landing the full stage or the engine only. As the optimisation criterion, the ratio of the specific launch cost of the reusable to the expendable version is used. The tool also provides for a Monte Carlo analysis, which allows for investigating the ruggedness of the design solution(s) found. The article will describe the methods implemented in the Conceptual Reusability Design Tool (CRDT) together with the modifications made to ParSim v3, a simulation tool by Delft Aerospace Rocket Engi- neering. Furthermore, it will present the steps taken to verify and validate CRDT. Finally, several example cases are presented based on the Atlas V-Centaur launch vehicle. The cases demonstrate the tools capa- bility of finding optimum and the sensitivity of the found optimum. However, it also shows the optimum when the user disables some Entry Descent and Landing (EDL) options. 1. Introduction To make space more accessible, one can reduce the cost of an orbital launch. -
Omega-3 Fatty Acids Fact Sheet for Consumers
Omega-3 Fatty Acids Fact Sheet for Consumers What are omega-3 fatty acids and what do they do? Omega-3 fatty acids are found in foods, such as fish and flaxseed, and in dietary supplements, such as fish oil. The three main omega-3 fatty acids are alpha-linolenic acid (ALA), eicosapentaenoic acid (EPA), and docosahexaenoic acid (DHA). ALA is found mainly in plant oils such as flaxseed, soybean, and canola oils. DHA and EPA are found in fish and other seafood. ALA is an essential fatty acid, meaning that your body can’t make it, so you must get it from the foods and beverages you consume. Your body can convert some ALA into EPA and then to DHA, but only in very small amounts. Therefore, getting EPA and DHA from foods (and dietary supplements if you take them) is the only practical way to increase levels of these omega-3 fatty acids in your body. Omega-3s are important components of the membranes that surround each cell in your body. DHA levels are especially high in retina (eye), brain, and sperm cells. Omega-3s also provide calories to give your body energy and have many functions in your heart, blood vessels, lungs, immune system, and endocrine system (the network of hormone-producing glands). How much omega-3s do I need? Omega-3s are found in foods Experts have not established recommended amounts for omega-3 fatty acids, except such as fatty fish and plant oils. for ALA. Average daily recommended amounts for ALA are listed below in grams (g). -
Falcon Heavy
Schaub 5:00 L04 Disclaimer: This paper partially fulfills a writing requirement for the first year (freshman) engineering students at the University of Pittsburgh Swanson School of Engineering. This paper is a student paper, not professional paper. This paper is based on publicly available information and may not provide complete analyses of all relevant data. If this paper is used for any purpose other than this author`s partial fulfillment of a writing requirement for first year (freshman) engineering students at the University of Pittsburgh Swanson School of Engineering, users are doing so at their own risk. FALCON HEAVY Zoë Neal ([email protected]) SPACEX order to finish the mission the vehicle was set out to SpaceX is a private space exploration do. company that designs and manufactures various Named after its use of nine first stage launch technologically advanced spacecraft and launch engineers, this is the world’s first partially reusable vehicles under the direction of co-founder and rocket [1]. It is comprised of three separate parts. CEO, Elon Musk [1]. The company was founded in The first stage is comprised of two boosters and the 2002 with the intent of advancing space exploration second stage is rocket itself. The Falcon 9 Full technology to achieve their ultimate goal of Thrust can lift cargo up to 50,300 pounds to low enabling humans to live on other planets. They are Earth orbit. That is the equivalent of sending a the first private company to return a spacecraft from sailboat, a greyhound bus, and a monster truck to an low-Earth orbit and are the first to use an orbital altitude of 1,200 miles.