Spacex Falcon 9 V1.2 Data Sheet Home on the Pad Space Logs Library Links Spacex Falcon 9 V1.2 Updated February 22, 2018
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The Annual Compendium of Commercial Space Transportation: 2013
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2013 February 2014 About FAA \ NOTICE ###i# £\£\ ###ii# Table of Contents TABLE OF CONTENTS INTRODUCTION. 1 YEAR AT A GLANCE ..............................................2 COMMERCIAL SPACE TRANSPORTATION 2013 YEAR IN REVIEW ........5 7 ORBITAL LAUNCH VEHICLES .....................................21 3 SUBORBITAL REUSABLE VEHICLES ...............................47 33 ON-ORBIT VEHICLES AND PLATFORMS ............................57 LAUNCH SITES .................................................65 COMMERCIAL VENTURES BEYOND EARTH ORBIT ...................79 44 REGULATION AND POLICY .......................................83 3 5 3 53 3 8599: : : ;55: 9 < 5; < 2013 COMMERCIAL SPACE TRANSPORTATION FORECASTS ..........89 4 3 4 : ACRONYMS AND ABBREVIATIONS ...............................186 2013 WORLDWIDE ORBITAL LAUNCH EVENTS .....................192 DEFINITIONS ..................................................196 ###iii# £\£\ LIST OF FIGURES COMMERCIAL SPACE TRANSPORTATION YEAR IN REVIEW = =999 =99 = =3> =:9;> LAUNCH SITES = :< 2013 COMMERCIAL SPACE TRANSPORTATION FORECASTS =944 =4 =?4;9 =99493 =3 =:5= =< =;=9 =95;@3 =A =;=9 A 3 =994?: =9999 ? =54 =359 =:5 3 =<999= ? =99=5 ?3 =;>>99: =99 ? 3 ==9 ? 3: =3 =>3 =?: =3?: =:? : ###iv# LIST OF TABLES COMMERCIAL SPACE TRANSPORTATION YEAR IN REVIEW 99 : 3< :9=99< <99 ORBITAL LAUNCH VEHICLES 99 99 59595 593 SUBORBITAL REUSABLE VEHICLES 3 :5933 ON-ORBIT VEHICLES -
By Tamman Montanaro
4 Reusable First Stage Rockets y1 = 15.338 m m1 = 2.047 x 10 kg 5 y2 = 5.115 m m2 = 1.613 x 10 kg By Tamman Montanaro What is the moment of inertia? What is the force required from the cold gas thrusters if we assume constancy. Figure 1. Robbert Goddard’s design of the first ever rocket to fly in 1926. Source: George Edward Pendray. The moment of inertia of a solid disk: rper The Rocket Formula Now lets stack a bunch of these solid disk on each other: Length = l Divide by dt Figure 2: Flight path for the Falcon 9; After separation, the first stage orientates itself and prepares itself for landing. Source: SpaceX If we do the same for the hollow cylinder, we get a moment of inertia Launch of: Specific impulse for a rocket: How much mass is lost? What is the mass loss? What is the moment of inertia about the center of mass for these two objects? Divide by m Figure 3: Falcon 9 first stage after landing on drone barge. Source: SpaceX nd On December 22 2015, the Falcon 9 Orbcomm-2 What is the constant force required for its journey halfway (assuming first stage lands successfully. This is the first ever orbital- that the force required to flip it 90o is the equal and opposite to class rocket landing. From the video and flight logs, we Flip Maneuver stabilize the flip). can gather specifications about the first stage. ⃑ How much time does it take for the first stage to descend? We assume this is the time it takes � Flight Specifications for the first stage to reorientate itself. -
MEDIA RELEASE Asiasat 8 Successfully Lifts Off
MEDIA RELEASE AsiaSat 8 Successfully Lifts Off Hong Kong, 5 August 2014 – AsiaSat 8 aboard a SpaceX Falcon 9 launch vehicle successfully lifted off from the Cape Canaveral Air Force Station in Florida, U.S.A. at Hong Kong Time 4:00 p.m. (4:00 a.m. EDT or Cape Canaveral local time) on the 5th of August. The spacecraft successfully separated from the launch vehicle 32 minutes after liftoff. AsiaSat has acquired the first signals from the satellite in Hong Kong 54 minutes after launch. Over the next few days, AsiaSat 8 will move into the geostationary orbit, some 36,000 km above the Equator. “We are excited that the AsiaSat 8 launch has achieved this significant milestone. This is our first launch with SpaceX, we would like to thank them for their excellent work and effort in making today’s launch a success. In the coming weeks, we will work closely with Space Systems/Loral, our long-term partner, on the post-launch maneuvers and in-orbit testing of AsiaSat 8,” said William Wade, President and Chief Executive Officer of AsiaSat. “The addition of AsiaSat 8 to our existing fleet of four in-orbit satellites will expand our fleet capacity and enable us to serve a wider range of customers for advanced satellite services, from DTH, data broadcasting to broadband services.” AsiaSat 8 is a Space Systems/Loral 1300 series satellite, and has a design life of 15 years. With 24 Ku-band transponders and a Ka-band payload, AsiaSat 8 will co-locate with AsiaSat 7, where AsiaSat has established networks for service since 1990. -
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; -
Annual Report 2014 Corporate Information
ABOUT AsiaSat Asia Satellite Telecommunications Holdings Limited (the “Company”) indirectly owns Asia Satellite Telecommunications Company Limited (“AsiaSat”) and other subsidiaries (collectively the “Group”) and is listed on The Stock Exchange of Hong Kong Limited (“Stock Exchange”) (Stock Code 1135). AsiaSat is Asia’s premier provider of high quality satellite services to the broadcasting and telecommunications markets. The Group owns six satellites that are located in prime geostationary positions over the Asian landmass and provide access to two-thirds of the world’s population. OUR VISION To be the foremost satellite solution provider in Asia and the instinctive and desired partner of choice. www.asiasat.com Contents 2 Financial Highlights 3 Corporate Information 4 Chairman’s Statement 10 Operations Review 14 Corporate Governance Report 30 Management Discussion and Analysis 35 Biographical Details of Directors and Senior Management 40 Directors’ Report 49 Audit Committee Report 50 Index to the Consolidated Financial Statements 112 Financial Summary 113 Independent Auditor’s Report 115 Shareholder Information Financial Highlights 2014 2013 Change Turnover HK$M 1,365 1,499 –9% Profits attributable to owners of the Company HK$M 559 748 –25% Dividend HK$M 223 947 –76% Capital and reserves HK$M 7,107 7,522 –6% Earnings per share HK cents 143 191 –25% Dividend per share HK cents 57 242 –76% Dividend cover Times 2.5 0.8 213% Return on equity Percent 8 10 –2% Net assets per share — book value HK cents 1,817 1,923 –6% 38 18 30 7 23 5 1,297 1,446 2 AsiaSat Annual Report 2014 Corporate Information CHAIRMAN AND NON-EXECUTIVE NOMINATION COMMITTEE DIRECTOR Maura WONG Hung Hung (Chairman) Sherwood P. -
Space Launch System (Sls) Motors
Propulsion Products Catalog SPACE LAUNCH SYSTEM (SLS) MOTORS For NASA’s Space Launch System (SLS), Northrop Grumman manufactures the five-segment SLS heavy- lift boosters, the booster separation motors (BSM), and the Launch Abort System’s (LAS) launch abort motor and attitude control motor. The SLS five-segment booster is the largest solid rocket motor ever built for flight. The SLS booster shares some design heritage with flight-proven four-segment space shuttle reusable solid rocket motors (RSRM), but generates 20 percent greater average thrust and 24 percent greater total impulse. While space shuttle RSRM production has ended, sustained booster production for SLS helps provide cost savings and access to reliable material sources. Designed to push the spent RSRMs safely away from the space shuttle, Northrop Grumman BSMs were rigorously qualified for human space flight and successfully used on the last fifteen space shuttle missions. These same motors are a critical part of NASA’s SLS. Four BSMs are installed in the forward frustum of each five-segment booster and four are installed in the aft skirt, for a total of 16 BSMs per launch. The launch abort motor is an integral part of NASA’s LAS. The LAS is designed to safely pull the Orion crew module away from the SLS launch vehicle in the event of an emergency on the launch pad or during ascent. Northrop Grumman is on contract to Lockheed Martin to build the abort motor and attitude control motor—Lockheed is the prime contractor for building the Orion Multi-Purpose Crew Vehicle designed for use on NASA’s SLS. -
IAC-17-D2.4.3 Page 1 of 18 IAC-17
68th International Astronautical Congress (IAC), Adelaide, Australia, 25-29 September 2017. Copyright ©2017 by DLR-SART. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-17- D2.4.3 Evaluation of Future Ariane Reusable VTOL Booster stages Etienne Dumonta*, Sven Stapperta, Tobias Eckerb, Jascha Wilkena, Sebastian Karlb, Sven Krummena, Martin Sippela a Department of Space Launcher Systems Analysis (SART), Institute of Space Systems, German Aerospace Center (DLR), Robert Hooke Straße 7, 28359 Bremen, Germany b Department of Spacecraft, Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Bunsenstraße 10, 37073 Gottingen, Germany *[email protected] Abstract Reusability is anticipated to strongly impact the launch service market if sufficient reliability and low refurbishment costs can be achieved. DLR is performing an extensive study on return methods for a reusable booster stage for a future launch vehicle. The present study focuses on the vertical take-off and vertical landing (VTOL) method. First, a restitution of a flight of Falcon 9 is presented in order to assess the accuracy of the tools used. Then, the preliminary designs of different variants of a future Ariane launch vehicle with a reusable VTOL booster stage are described. The proposed launch vehicle is capable of launching a seven ton satellite into a geostationary transfer orbit (GTO) from the European spaceport in Kourou. Different stagings and propellants (LOx/LH2, LOx/LCH4, LOx/LC3H8, subcooled LOx/LCH4) are considered, evaluated and compared. First sizing of a broad range of launcher versions are based on structural index derived from existing stages. -
Status of the Space Shuttle Solid Rocket Booster
The Space Congress® Proceedings 1980 (17th) A New Era In Technology Apr 1st, 8:00 AM Status of The Space Shuttle Solid Rocket Booster William P. Horton Solid Rocket Booster Engineering Office, George C. Marshall Space Flight Center, Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Horton, William P., "Status of The Space Shuttle Solid Rocket Booster" (1980). The Space Congress® Proceedings. 3. https://commons.erau.edu/space-congress-proceedings/proceedings-1980-17th/session-1/3 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]. STATUS OF THE SPACE SHUTTLE SOLID ROCKET BOOSTER William P. Horton, Chief Engineer Solid Rocket Booster Engineering Office George C. Marshall Space Flight Center, AL 35812 ABSTRACT discuss retrieval and refurbishment plans for Booster reuse, and will address Booster status Two Solid Rocket Boosters provide the primary for multimission use. first stage thrust for the Space Shuttle. These Boosters, the largest and most powerful solid rocket vehicles to meet established man- BOOSTER CONFIGURATION rated design criteria, are unique in that they are also designed to be recovered, refurbished, It is appropriate to review the Booster config and reused. uration before describing the mission profile. The Booster is 150 feet long and is 148 inches The first SRB f s have been stacked on the in diameter (Figure 1), The inert weight Mobile Launch Platform at the Kennedy Space is 186,000 pounds and the propellant weight is Center and are ready to be mated with the approximately 1.1 million pounds for each External Tank and Orbiter in preparation for Booster. -
FEDERAL COMMUNICATIONS COMMISSION in the Matter Of
Before the FEDERAL COMMUNICATIONS COMMISSION Washington, D.C. 20554 In the Matter of Expanding Flexible Use of the 3.7 GHz to 4.2 GN Docket No. 18-122 GHz Band Eligible Satellite Operator Transition Plans for GN Docket No. 20-173 the 3.7-4.2 GHz Band REVISED TRANSITION PLAN OF EUTELSAT S.A. Pursuant to Section 27.1412(d) of the Commission’s rules,1 Eutelsat S.A. (“Eutelsat”) hereby submits this Revised Transition Plan incorporating updated information and feedback from the Commission staff in describing the process it intends to follow to effect the relocation of its fixed-satellite service customers out of the 3.7-4.0 GHz band in the contiguous United States (“CONUS”), as required by the Commission’s C-band Order in the above-captioned proceeding. Eutelsat has separately filed a Petition for Expedited Reconsideration or Clarification, in which it has requested that the Commission confirm that eligible replacement satellite costs are limited to satellites operating only in the 4.0-4.2 GHz band (and corresponding uplink band) and covering only the CONUS. Eutelsat further requested that the Commission requires each such subsidized satellite to serve the CONUS for the duration of its useful life, and that the Commission specifically clarifies that the costs of spare satellites and “backup” launches are ineligible.2 Eutelsat continues to urge the Commission to act on that Petition, in order to bring greater clarity and consistency to the process under which C-band satellite operators are developing these Transition Plans. 1 47 C.F.R. -
Grand Challenges and Vast Opportunities
Near Term Space Settlement: Risk Reduction Missions Kent Nebergall Macroinvent.com Mars Society Conference, 2017 © 2017 Kent Nebergall All rights reserved. The Grand Challenges of Space Settlement (2014) Launch/LEO Deep Space Moon/Mars Settlement Affordable Launch Solar Flares Moon Landing Air/Water Large Vehicle Launch GCR: Cell Damage Mars EDL Fuel Mass Fraction beyond Medication/ Spacesuit Lifespan Power Earth Orbit (Refueling) Food Expiration Space Junk Life Support Closed Reliable Ascent Vehicle Food Loop Microgravity Medical Entropy Reliable Return Vehicle Assembly (health issues) in Orbit Psychology Flight to Earth Mining Mechanical Entropy Earth Reentry Manufacture Funded Projects NASA Focus Commercial Focus Gaps © 2017 Kent Nebergall All rights reserved. Preparing for the NewSpace Revolution Year Energy Information Invention Affordability 2017 Falcon 9 Block 5 Falcon Heavy 2018 Crewed Dragon Blockchain Matures Crewed Starliner 2019 LEO Internet 2020 Low Latency Global Bigelow BA330 New Glenn Internet Satellites 50 MT satellites have two 2021 Quantum Computing? launch platforms, both AI Capabilities cheap and rapid NASA Space turnaround ISS Replacement 2022 Nuclear Power Groundwork Nuclear propulsion © 2017 Kent Nebergall All rights reserved. NASA Nuclear Projects BWXT Nuclear Thermal Rocket TDU 10-100 KW KiloPower 1-10 KW © 2017 Kent Nebergall All rights reserved. Driving Critical Mass for the NewSpace Revolution • Deep Space Risk Reduction Missions • Organizing for Direct Solutions Deep Space DragonLab 1 • Exposure test items that are altered when exposed to deep space to test the risk • Launch into high (lunar distance apogee) orbit to expose to unfiltered cosmic rays and solar flares • After mission simulating full trip to/on/from Mars, return the cargo and examine results. -
59864 Federal Register/Vol. 85, No. 185/Wednesday, September 23
59864 Federal Register / Vol. 85, No. 185 / Wednesday, September 23, 2020 / Rules and Regulations FEDERAL COMMUNICATIONS C. Congressional Review Act II. Report and Order COMMISSION 2. The Commission has determined, A. Allocating FTEs 47 CFR Part 1 and the Administrator of the Office of 5. In the FY 2020 NPRM, the Information and Regulatory Affairs, Commission proposed that non-auctions [MD Docket No. 20–105; FCC 20–120; FRS Office of Management and Budget, funded FTEs will be classified as direct 17050] concurs that these rules are non-major only if in one of the four core bureaus, under the Congressional Review Act, 5 i.e., in the Wireline Competition Assessment and Collection of U.S.C. 804(2). The Commission will Bureau, the Wireless Regulatory Fees for Fiscal Year 2020 send a copy of this Report & Order to Telecommunications Bureau, the Media Congress and the Government Bureau, or the International Bureau. The AGENCY: Federal Communications indirect FTEs are from the following Commission. Accountability Office pursuant to 5 U.S.C. 801(a)(1)(A). bureaus and offices: Enforcement ACTION: Final rule. Bureau, Consumer and Governmental 3. In this Report and Order, we adopt Affairs Bureau, Public Safety and SUMMARY: In this document, the a schedule to collect the $339,000,000 Homeland Security Bureau, Chairman Commission revises its Schedule of in congressionally required regulatory and Commissioners’ offices, Office of Regulatory Fees to recover an amount of fees for fiscal year (FY) 2020. The the Managing Director, Office of General $339,000,000 that Congress has required regulatory fees for all payors are due in Counsel, Office of the Inspector General, the Commission to collect for fiscal year September 2020. -
Spacex Rocket Data Satisfies Elementary Hohmann Transfer Formula E-Mail: [email protected] and [email protected]
IOP Physics Education Phys. Educ. 55 P A P ER Phys. Educ. 55 (2020) 025011 (9pp) iopscience.org/ped 2020 SpaceX rocket data satisfies © 2020 IOP Publishing Ltd elementary Hohmann transfer PHEDA7 formula 025011 Michael J Ruiz and James Perkins M J Ruiz and J Perkins Department of Physics and Astronomy, University of North Carolina at Asheville, Asheville, NC 28804, United States of America SpaceX rocket data satisfies elementary Hohmann transfer formula E-mail: [email protected] and [email protected] Printed in the UK Abstract The private company SpaceX regularly launches satellites into geostationary PED orbits. SpaceX posts videos of these flights with telemetry data displaying the time from launch, altitude, and rocket speed in real time. In this paper 10.1088/1361-6552/ab5f4c this telemetry information is used to determine the velocity boost of the rocket as it leaves its circular parking orbit around the Earth to enter a Hohmann transfer orbit, an elliptical orbit on which the spacecraft reaches 1361-6552 a high altitude. A simple derivation is given for the Hohmann transfer velocity boost that introductory students can derive on their own with a little teacher guidance. They can then use the SpaceX telemetry data to verify the Published theoretical results, finding the discrepancy between observation and theory to be 3% or less. The students will love the rocket videos as the launches and 3 transfer burns are very exciting to watch. 2 Introduction Complex 39A at the NASA Kennedy Space Center in Cape Canaveral, Florida. This launch SpaceX is a company that ‘designs, manufactures and launches advanced rockets and spacecraft.