Analysis of Human-Machine Interfaces and Systems in Space Christine
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Vulcan Centaur
VULCAN CENTAUR The Vulcan Centaur rocket design leverages the flight-proven success of the Delta IV and Atlas V launch vehicles while introducing new technologies and innovative features to ensure a reliable and aordable space launch service. Vulcan Centaur will service a diverse range of markets including 225 ft commercial, civil, science, cargo and national security space customers. 1 The spacecraft is encapsulated in a 5.4-m- (17.7-ft-) diameter payload fairing (PLF), a sandwich composite structure made with a vented aluminum-honeycomb core and graphite-epoxy face sheets. The bisector (two-piece shell) PLF encapsulates the spacecraft. The payload attach fitting (PAF) is a similar sandwich composite structure creating the mating interface from spacecraft to second stage. The PLF separates using a debris-free horizontal and vertical separation system with 2 200 ft spring packs and frangible joint assembly. The payload fairing is available in the 15.5-m (51-ft) standard and 21.3-m (70-ft) 1 long configurations. The Centaur upper stage is 5.4 m (17.7 ft) in diameter and 3 11.7 m (38.5 ft) long with a 120,000-lb propellant capacity. Its propellant tanks are constructed of pressure-stabilized, corrosion-resistant stainless steel. Centaur is a liquid hydrogen/liquid oxygen-fueled vehicle, with two RL10C 4 engines. The Vulcan Centaur Heavy vehicle, flies the upgraded 2 Centaur using RL10CX engines with nozzle extensions. The 5 175 ft cryogenic tanks are insulated with spray-on foam insulation (SOFI) to manage boil o of cryogens during flight. An aft equipment shelf provides the structural mountings for vehicle electronics. -
Aerospace Dimensions Leader's Guide
Leader Guide www.capmembers.com/ae Leader Guide for Aerospace Dimensions 2011 Published by National Headquarters Civil Air Patrol Aerospace Education Maxwell AFB, Alabama 3 LEADER GUIDES for AEROSPACE DIMENSIONS INTRODUCTION A Leader Guide has been provided for every lesson in each of the Aerospace Dimensions’ modules. These guides suggest possible ways of presenting the aerospace material and are for the leader’s use. Whether you are a classroom teacher or an Aerospace Education Officer leading the CAP squadron, how you use these guides is up to you. You may know of different and better methods for presenting the Aerospace Dimensions’ lessons, so please don’t hesitate to teach the lesson in a manner that works best for you. However, please consider covering the lesson outcomes since they represent important knowledge we would like the students and cadets to possess after they have finished the lesson. Aerospace Dimensions encourages hands-on participation, and we have included several hands-on activities with each of the modules. We hope you will consider allowing your students or cadets to participate in some of these educational activities. These activities will reinforce your lessons and help you accomplish your lesson out- comes. Additionally, the activities are fun and will encourage teamwork and participation among the students and cadets. Many of the hands-on activities are inexpensive to use and the materials are easy to acquire. The length of time needed to perform the activities varies from 15 minutes to 60 minutes or more. Depending on how much time you have for an activity, you should be able to find an activity that fits your schedule. -
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; -
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. -
Annual Report of S.P
ANNUAL REPORT OF S.P. KOROLEV ROCKET AND SPACE PUBLIC CORPORATION ENERGIA FOR 2019 This Annual Report of S.P.Korolev Rocket and Space Public Corporation Energia (RSC Energia) was prepared based upon its performance in 2019 with due regard for the requirements stated in the Russian Federation Government Decree of December 31, 2010 No. 1214 “On Improvement of the Procedure to Control Open Joint-Stock Companies whose Stock is in Federal Ownership and Federal State Unitary Enterprises”, and in accordance with the Regulations “On Information Disclosure by the Issuers of Outstanding Securities” No. 454-P approved by the Bank of Russia on December 30, 2014 Accuracy of the data contained in this Annual Report, including the Report on the interested-party transactions effected by RSC Energia in 2019, was confirmed by RSC Energia’s Auditing Committee Report as of 01.06.2020. This Annual Report was preliminary approved by RSC Energia’s Board of Directors on August 24, 2020 (Minutes No. 31). This Annual Report was approved at RSC Energia’s General Shareholders’ Meeting on September 28, 2020 (Minutes No 40 of 01.10.2020). 2 TABLE OF CONTENTS 1. BACKGROUND INFORMATION ABOUT RSC ENERGIA ............................. 6 1.1. Company background .........................................................................................................................6 1.2. Period of the Company operation in the industry ...............................................................................6 1.3. Information about the purchase and sale contracts for participating interests, equities, shares of business partnerships and companies concluded by the Company in 2019 ..............................................7 1.4. Information about the holding structure and the organizations involved ...........................................8 2. PRIORITY DIRECTIONS OF RSC ENERGIA OPERATION ........................ 11 2.1. -
The International Space Station and the Space Shuttle
Order Code RL33568 The International Space Station and the Space Shuttle Updated November 9, 2007 Carl E. Behrens Specialist in Energy Policy Resources, Science, and Industry Division The International Space Station and the Space Shuttle Summary The International Space Station (ISS) program began in 1993, with Russia joining the United States, Europe, Japan, and Canada. Crews have occupied ISS on a 4-6 month rotating basis since November 2000. The U.S. Space Shuttle, which first flew in April 1981, has been the major vehicle taking crews and cargo back and forth to ISS, but the shuttle system has encountered difficulties since the Columbia disaster in 2003. Russian Soyuz spacecraft are also used to take crews to and from ISS, and Russian Progress spacecraft deliver cargo, but cannot return anything to Earth, since they are not designed to survive reentry into the Earth’s atmosphere. A Soyuz is always attached to the station as a lifeboat in case of an emergency. President Bush, prompted in part by the Columbia tragedy, made a major space policy address on January 14, 2004, directing NASA to focus its activities on returning humans to the Moon and someday sending them to Mars. Included in this “Vision for Space Exploration” is a plan to retire the space shuttle in 2010. The President said the United States would fulfill its commitments to its space station partners, but the details of how to accomplish that without the shuttle were not announced. The shuttle Discovery was launched on July 4, 2006, and returned safely to Earth on July 17. -
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 ......................................................................... -
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. -
Why It Could Be Time to Shoot for a Scramjet Big Enough to Do
AIAA PRESIDENTIAL ELECTION 18 MODELING 42 COMMERCIAL SPACE 10 The candidates speak The state of CFD Axiom’s Ondler on station planning Scaling up Why it could be time to shoot for a scramjetPAGE 22 big enough to do something big JANUARY 2021 | A publication of the American Institute of Aeronautics and Astronautics | aerospaceamerica.aiaa.org SPACE AND MISSILES SPACE AND MISSILES Crewed launch returns SpaceX launched its 100th mission in August, and in April its Falcon 9 rocket became the most to Kennedy Space Center fl own active rocket with its 84th launch. An August launch of a Falcon 9 fl ew a booster core for a record BY DALE ARNEY sixth time; a Falcon 9 payload fairing was reused for The Space Transportation Technical Committee works to foster continuous the fi rst time in November 2019. SpaceX performed improvements to civil, commercial and military launch vehicles. 150-meter test fl ights in August and September of its Starship prototype at its south Texas facility. .S. astronauts were launched from NASA’s ULA in July launched NASA’s Perseverance rover Kennedy Space Center in Florida for the to Mars on an Atlas V rocket. Blue Origin delivered fi rst time since 2011. For the Demo-2 mis- a pathfi nder BE-4 engine, and Northrop Grumman Usion, Bob Behnken and Doug Hurley fl ew to completed the fi rst qualifi cation test for a strap- the International Space Station aboard a SpaceX on booster. Both are being developed for ULA’s Crew Dragon capsule atop a Falcon 9 rocket in next-generation rocket, Vulcan Centaur. -
Columbia Accident Investigation Board
COLUMBIA ACCIDENT INVESTIGATION BOARD Report Volume I August 2003 COLUMBIA ACCIDENT INVESTIGATION BOARD On the Front Cover This was the crew patch for STS-107. The central element of the patch was the microgravity symbol, µg, flowing into the rays of the Astronaut symbol. The orbital inclination was portrayed by the 39-degree angle of the Earthʼs horizon to the Astronaut symbol. The sunrise was representative of the numerous science experiments that were the dawn of a new era for continued microgravity research on the International Space Station and beyond. The breadth of science conduct- ed on this mission had widespread benefits to life on Earth and the continued exploration of space, illustrated by the Earth and stars. The constellation Columba (the dove) was chosen to symbolize peace on Earth and the Space Shuttle Columbia. In addition, the seven stars represent the STS-107 crew members, as well as honoring the original Mercury 7 astronauts who paved the way to make research in space possible. The Israeli flag represented the first person from that country to fly on the Space Shuttle. On the Back Cover This emblem memorializes the three U.S. human space flight accidents – Apollo 1, Challenger, and Columbia. The words across the top translate to: “To The Stars, Despite Adversity – Always Explore“ Limited First Printing, August 2003, by the Columbia Accident Investigation Board Subsequent Printing and Distribution by the National Aeronautics and Space Administration and the Government Printing Office Washington, D.C. 2 Report Volume I August 2003 COLUMBIA ACCIDENT INVESTIGATION BOARD IN MEMORIAM Rick D. Husband Commander William C. -
STS-132 Mission Summary
NASA Mission Summary National Aeronautics and Space Administration Washington, D.C. 20546 (202) 358-1100 STS-132 MISSION SUMMARY May 2010 SPACE SHUTTLE ATLANTIS Atlantis’ 12-day mission will deliver the Russian-built Mini Research Module-1 that will provide additional storage space and a new docking port for Russian Soyuz and Progress spacecraft. MRM-1, also known as Rassvet, which means dawn in Russian, will be permanently attached to the bottom port of the station’s Zarya module. MRM-1 will carry important hardware on its exterior including a radiator, airlock and a European robotic arm. Atlantis also will deliver addi- tional station hardware stored inside a cargo carrier. Three spacewalks are planned to stage spare components outside the station, including six spare batteries, a Ku-band antenna and spare parts for the Canadian Dextre robotic arm. Shuttle mission STS-132 is the final sched- uled flight for Atlantis . CREW Ken Ham Tony Antonelli (an-tuh-NEL-lee) Commander (Captain, U.S. Navy) Pilot (Commander, U.S. Navy) ● Veteran of one spaceflight, STS-124 pilot ● Veteran of one spaceflight, STS-119 pilot ● Age: 45, Born: Plainfield, N.J. ● Born: Detroit ● Married with two children ● Married with two children ● Logged 5,000+ hours in 40 different aircraft ● Logged 3,200+ hours in 41 different aircraft ● Call sign: Hock ● Interests include snow boarding and NASCAR Garrett Reisman (REESE-man) Michael Good Mission Specialist-1 Mission Specialist-2 (Col., U.S. Air Force, Ret.) ● Veteran flight engineer on Expedition 16 & 17 ● Veteran of one spaceflight, STS-125 ● Launched on STS-123; returned STS-124 ● Age: 47, Hometown: Broadview Heights, Ohio ● Age: 42, Hometown: Parsippany, N.J. -
Vulcan Centaur Rocket with Your Printer and Basic Tools
VULCAN CENTAUR Paper Model Kit VULCAN CENTAUR This paper rocket kit is a designed to help you build a 1:150 scale model of the Vulcan Centaur rocket with your printer and basic tools. As with all paper model kits, your level of success will depend on your precision and the time you take. It is recommended to let the glue fully dry in each step before the next. Please take care not to cut yourself and do not leave children unattended with sharp tools. Your Vulcan Centaur paper model kit will require: • 8.5” x 11” cardstock prints of the 4 pages at the end of this document, (save paper and ink by only print- ing the pattern pages 13-16 and view the instructions online) • A cutting mat • Scissors and/or an x-acto knife (children should not use x-acto or be left unattended with cutting tools and anyone attempting this kit should take care to avoid injury from cuts) • Glue (super glue or other adhesive is not necessary) • A straight edge or ruler Optional supplies: • A few toothpicks for applying glue to small areas • A small dish to hold a dollop of glue while building • A long wooden dowel or chopstick to help you apply pressure to glued areas far into the rocket body • A sharpened pencil STEP 1 Mark the booster (A) for solid rocket boosters before cutting Vulcan Centaur has the capability of using 0, 2, 4 or 6 solid rocket boosters (SRBs) for added performance. You will mark the locations for the SRBs first.