Thirty-Five Years in Power for America
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Privacy Statement Link at the Bottom of Aerojet Rocketdyne Websites
Privacy Notice Aerojet Rocketdyne – For external use Contents Introduction ...................................................................................................................... 3 Why we collect personal information? ............................................................................. 3 How we collect personal information? ............................................................................. 3 How we use information we collect? ............................................................................... 4 How we share your information? .................................................................................... 4 How we protect your personal information? ..................................................................... 4 How we collect consent? .............................................................................................. 4 How we provide you access? ........................................................................................ 4 How to contact Aerojet Rocketdyne privacy?.................................................................... 5 Collection of personal information .................................................................................. 5 Disclosure of personal information.................................................................................. 5 Sale of personal information .......................................................................................... 6 Children’s online privacy .............................................................................................. -
Materials for Liquid Propulsion Systems
https://ntrs.nasa.gov/search.jsp?R=20160008869 2019-08-29T17:47:59+00:00Z CHAPTER 12 Materials for Liquid Propulsion Systems John A. Halchak Consultant, Los Angeles, California James L. Cannon NASA Marshall Space Flight Center, Huntsville, Alabama Corey Brown Aerojet-Rocketdyne, West Palm Beach, Florida 12.1 Introduction Earth to orbit launch vehicles are propelled by rocket engines and motors, both liquid and solid. This chapter will discuss liquid engines. The heart of a launch vehicle is its engine. The remainder of the vehicle (with the notable exceptions of the payload and guidance system) is an aero structure to support the propellant tanks which provide the fuel and oxidizer to feed the engine or engines. The basic principle behind a rocket engine is straightforward. The engine is a means to convert potential thermochemical energy of one or more propellants into exhaust jet kinetic energy. Fuel and oxidizer are burned in a combustion chamber where they create hot gases under high pressure. These hot gases are allowed to expand through a nozzle. The molecules of hot gas are first constricted by the throat of the nozzle (de-Laval nozzle) which forces them to accelerate; then as the nozzle flares outwards, they expand and further accelerate. It is the mass of the combustion gases times their velocity, reacting against the walls of the combustion chamber and nozzle, which produce thrust according to Newton’s third law: for every action there is an equal and opposite reaction. [1] Solid rocket motors are cheaper to manufacture and offer good values for their cost. -
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Frontierswww.boeing.com/frontiers JUNEJULY 20092009 // VolumeVolume VIII,VIII, IssueIssue IIIII wingsNew ScanEagle leads Boeing future in unmanned airborne systems market JULY 2009 / BOEING FRONTIERS BOEING FRONTIERS / JULY 2009 / VOLUME VIII, ISSUE III On the Cover 14 Flying into the future Innovative unmanned aircraft systems such as ScanEagle, developed by Boeing subsidiary Insitu, are helping Boeing expand in one of the fastest-growing markets in aerospace. COVER IMAGE: TRAVIS CIELOHA OF INSITU, WITH THE SCANEAGLE UNMANNED AIRCRAFT SYSTEM. CDR DOUG KIEM/U.S. NAVY PHOTO: SCANEAGLE IN FLIGHT. CDR DOUG KIEM/U.S. NAVY BOEING FRONTIERS / JULY 2009 / VOLUME VIII, ISSUE III 3 Safer air travel Frontiers Flying today is safer than ever, thanks in large part to the Commercial Publisher: Tom Downey 12 Aviation Safety Team. Working together, representatives from industry, Editorial director: Anne Toulouse government, unions and academia developed and promoted safety initiatives that have improved aviation safety around the globe. EDITORIAL TEAM The team’s efforts recently were recognized with the prestigious Editor: Collier Trophy. Paul Proctor: 312-544-2938 Managing editor (acting): Ann Beach: 312-544-2997 Deputy managing editor: Vineta Plume: 312-544-2954 Out of this world Art director: Brandon Luong: 312-544-2118 For Boeing Mission Control Center employees who design, build and test satellites, the launch is just the beginning. Then comes the critical Commercial Airplanes editor: 24 work of satellite operations. Julie O’Donnell: 206-766-1329 Engineering, Operations & Technology editor: Junu Kim: 312-544-2939 Human Resources and Administration editor: Geoff Potter: 312-544-2946 Apollo 11: A walk to remember Integrated Defense Systems editor: Two Boeing engineers—then a new engineering school graduate and a Diane Stratman: 562-797-1443 28 teenager with lofty aspirations—share the challenges and excitement of Shared Services editor: launching the Apollo 11 mission that put man on the moon 40 years ago Beriah Osorio: 425-577-4157 this summer. -
Download of Your Pictures to Your Computer
w ww om .estesrockets.c TABLE OF CONTENTS Index . .2 Skill Level 2 Rocket Kits . .26 How To Start . .3 Skill Level 3 Rocket Kits . .30 What to Know . .4 “E” Engine Powered Kits . .32 Model Rocket Safety Code . .5 Blurzz™ Rocket Racers . .33 Ready To Fly Starter Sets . .6 How Model Rocket Engines Work . .34 E2X® Starter Sets . .8 Model Rocket Engine Chart . .35 Ready to Fly Launch Sets . .10 Engine Time/Thrust Curves . .36 E2X® Launch Sets . .12 Model Rocket Accessories . .37 Ready To Fly Rockets . .14 Estes Airplanes . .38 E2X® Rocket Kits . .15 Estes Educator™ Products . .41 Skill Level 1 Rocket Kits . .20 Estes Specialty Products . .42 INDEX 220 Swift™. 21 Lucky Seven . 17 36 D Squared™ . 27 Max Trax® Starter Set. 7 Accessories. 37 Mini Super Shot™ Starter Set . 9 AeroX™ Interceptor™R/C Mobile Launcher. 40 Model Rocket Bulk Packs . 41 Air Force 1 Electric R/C Jet. 39 No. 2 Estes Sky Writer® . 17 Air Powered Action Hero. 43 NSA Starship™ . 7 Air Powered Blast Jets®. 43 Operation Search & Destroy™ Launch Set . 11 Air Show™ Launch Set. 13 Oracle™ Digital Camera Rocket . 19 Alpha®. 21 Outlander™ . 31 Alpha III®. 17 Patriot™ Starter Set. 7 Alpha III® Starter Set . 9 Presidential VIP Electric R/C Jet Airplane. 39 Astrocam® 110 . 19 Quickfire™ Catapult R/C Airplane . 39 Baby Bertha™. 21 Quark™ . 21 Bandito™ . 15 Renegade™ . 31 Big Bertha® . 23 Riptide™ Launch Set. 11 Big Daddy™ . 32 Rocket Bulk Packs. 41 Blue Ninja™ . 17 Rubicon . 25 Blurzz™ Rocket Powered Cars . 33 Scissor Wing Transport™ . 31 Bull Pup 12D™. -
ADVANCED SPACE ENGINE N74-16489 PRELIINABY DESIGN (Rocketdyne) F5,-P HC CSCL 21H $27.25 Unclas G3/28 28289 1
NASA CR-121236 R-9269 ADVANCED SPACE ENGINE PRELIMINARY DESIGN By A. T. Zachary ROCKETDYNE DIVISION C- ROCKWELL INTERNATIONAL Prepared for NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA-Lewis Research Center Contract NAS3-16751 (NVSA-CR-121236) ADVANCED SPACE ENGINE N74-16489 PRELIINABY DESIGN (Rocketdyne) f5,-p HC CSCL 21H $27.25 Unclas G3/28 28289 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA CR-121236 4. Title and Subtitle 5. Report Date ADVANCED SPACE ENGINE PRELIMINARY DESIGN October 1973 6. Performing Organization Code 7. Author(s) 8. Performing Organization Report No. A.T. Zachary R-9269 10. Work Unit No. 9. Performing Organization Name and Address Rocketdyne Division, Rockwell International 11. Contract or Grant No. Canoga Park, California, 91304 NAS3-16751 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Contractor Report National Aeronautics and Space Administration Washington, D.C., 20546 14. Sponsoring Agency Code 15. Supplementary Notes Project Manager, D.D. Scheer, NASA-Lewis Research Center, Cleveland, Ohio 16. Abstract Analysis and design of an optimum LO2/LH2, combustion topping cycle, 88,964 N (20,000-pound) thrust, liquid rocket engine was conducted. The design selected is well suited to high-energy, upper-stage engine applications such as the Space Tug and embodies features directed toward optimization of vehicle performance. A configuration selection was conducted based on prior Air Force Contracts F04611-71-C0039, F04611-71-C-0040, and F04611-67-C-0016,.and additional criteria for optimum stage performance. Following configuration selection, analyses and design of the major components and engine systems were conducted to sufficient depth to provide layout drawings suitable for subsequent detailing. -
NWIRP Dallas Is an Aerospace Manufacturing Complex Constructed in 1941 As Part of the U.S
I NTEGRATED C ULTURAL R ESOURCES M ANAGEMENT P LAN HISTORIC CONTEXT INTRODUCTION NWIRP Dallas is an aerospace manufacturing complex constructed in 1941 as part of the U.S. World War II Industrial Mobilization Program. Known as Plancor #25, NWIRP Dallas initially consisted of 85 buildings and structures spread out over 153 acres in rural Dallas County, near the city limits of both Dallas and Grand Prairie, Texas. The original project owner, the DPC, was a governmental body assigned to fund and build a variety of industrial facilities across the United States that produced essential military goods for World War II. North American Aviation Inc. leased the government- owned plant from 1941 to August 1945, producing nearly 30,000 aircraft of three different types for the Army, Air Force, and Navy. NWIRP Dallas has been leased to six different tenants over the past six decades: North American Aviation, TEMCO, Chance Vought Aircraft Corporation, LTV, Northrop Grumman, and Vought Aircraft Industries. Today, the complex consists of 343 resources on 314.66 acres. NWIRP Dallas has a complicated but important history that details the role it played during the Second World War and its significance throughout the Cold War. Its history is not only the story of an aircraft plant but also of the growth of Dallas County and the aircraft industry in North Texas communities. WORLD WAR II In the mid-1930s, there were definite signs that the peace established in Europe following World War I was tenuous. The first indication of trouble appeared in 1933 when Germany elected Adolf Hitler as its Chancellor and demanded equality with France and England, not disarmament. -
Space Shuttle Main Engine Orientation
BC98-04 Space Transportation System Training Data Space Shuttle Main Engine Orientation June 1998 Use this data for training purposes only Rocketdyne Propulsion & Power BOEING PROPRIETARY FORWARD This manual is the supporting handout material to a lecture presentation on the Space Shuttle Main Engine called the Abbreviated SSME Orientation Course. This course is a technically oriented discussion of the SSME, designed for personnel at any level who support SSME activities directly or indirectly. This manual is updated and improved as necessary by Betty McLaughlin. To request copies, or obtain information on classes, call Lori Circle at Rocketdyne (818) 586-2213 BOEING PROPRIETARY 1684-1a.ppt i BOEING PROPRIETARY TABLE OF CONTENT Acronyms and Abbreviations............................. v Low-Pressure Fuel Turbopump............................ 56 Shuttle Propulsion System................................. 2 HPOTP Pump Section............................................ 60 SSME Introduction............................................... 4 HPOTP Turbine Section......................................... 62 SSME Highlights................................................... 6 HPOTP Shaft Seals................................................. 64 Gimbal Bearing.................................................... 10 HPFTP Pump Section............................................ 68 Flexible Joints...................................................... 14 HPFTP Turbine Section......................................... 70 Powerhead........................................................... -
AEHF-6 Launch Marks 500Th Flight of Aerojet Rocketdyne's RL10 Engine
AEHF-6 Launch Marks 500th Flight of Aerojet Rocketdyne’s RL10 Engine March 27, 2020 CAPE CANAVERAL, Fla., March 26, 2020 (GLOBE NEWSWIRE) -- The successful March 26 launch of the U.S. Space Force’s sixth and final Advanced Extremely High Frequency (AEHF) military communications satellite aboard a United Launch Alliance (ULA) Atlas V rocket marked the 500th flight of Aerojet Rocketdyne’s RL10 upper-stage engine. The RL10, which powers the ULA Atlas V Centaur upper stage, is one of several Aerojet Rocketdyne propulsion products supporting the mission. Aerojet Rocketdyne propulsion can be found on both the rocket and the AEHF-6 satellite. Built by Lockheed Martin, the AEHF satellites provide secure, jam-proof communications, including nuclear command and control, to U.S. and allied forces. “This launch marks an important milestone for Aerojet Rocketdyne and for the country,” said Eileen Drake, Aerojet Rocketdyne’s CEO and president. “The RL10 has supported a majority of the nation’s most important national security and scientific missions, including all of the AEHF satellites which provide communication links that are critical to our warfighters.” The Atlas V in the 551 configuration is the most powerful vehicle in the Atlas V family, featuring five Aerojet Rocketdyne AJ-60A solid rocket strap-on motors, each generating 348,500 pounds of thrust. Designed specifically to provide extra lifting power to the Atlas V, the AJ-60A is the world’s largest monolithic solid rocket motor ever flown. The AEHF-6 satellite, meanwhile, is outfitted with three different types of Aerojet Rocketdyne thrusters for attitude control, orbital station keeping and maneuvering. -
SLS Case Study
CASE STUDY Supporting Space Flight History with the Space Launch System (SLS) Technetics Group is a proud sup- Boeing representatives held a sup- plier to NASA, Boeing and Aerojet plier recognition presentation for Rocketdyne, and proved instru- the Technetics team members, mental in working with these orga- citing outstanding performance nizations on the development of in providing hydraulic accumula- NASA’s Space Launch System (SLS). tors and reservoirs for the Thrust The SLS is an advanced, heavy-lift Vector Control hydraulic system, BELFAB Edge-Welded launch vehicle that will send astro- located within the Core Stage of Metal Bellows nauts into deep space and open the rocket. Technetics was one up the possibility for missions to of the first suppliers on the pro- Qualiseal Mechanical neighboring planets. The program gram to have provided all Flight 1 Seals is enabling humans to travel fur- requirements and subsystem test ther into space than ever before units. and paving the way for new sci- Aerojet Rocketdyne also rec- entific discoveries and knowledge ognized Technetics and stated that was once out of reach. that Technetics “has gone above Technetics has worked closely and beyond to produce quality with program design teams for hardware and support aggressive critical applications for the Core schedules,” and that “Technetics Stage and Upper Stage on the SLS. efforts and those of Technetics NAFLEX Seals Specifically, a number of preci- employees have not gone unno- sion sealing solutions and fluid ticed.” To express their appre- management components were ciation, Aerojet Rocketdyne needed for Aerojet Rocketdyne’s representatives visited the RS-25 and RL10 engines to ensure Technetics Deland, FL facility to the integrity of the overall system. -
Apollo Rocket Propulsion Development
REMEMBERING THE GIANTS APOLLO ROCKET PROPULSION DEVELOPMENT Editors: Steven C. Fisher Shamim A. Rahman John C. Stennis Space Center The NASA History Series National Aeronautics and Space Administration NASA History Division Office of External Relations Washington, DC December 2009 NASA SP-2009-4545 Library of Congress Cataloging-in-Publication Data Remembering the Giants: Apollo Rocket Propulsion Development / editors, Steven C. Fisher, Shamim A. Rahman. p. cm. -- (The NASA history series) Papers from a lecture series held April 25, 2006 at the John C. Stennis Space Center. Includes bibliographical references. 1. Saturn Project (U.S.)--Congresses. 2. Saturn launch vehicles--Congresses. 3. Project Apollo (U.S.)--Congresses. 4. Rocketry--Research--United States--History--20th century-- Congresses. I. Fisher, Steven C., 1949- II. Rahman, Shamim A., 1963- TL781.5.S3R46 2009 629.47’52--dc22 2009054178 Table of Contents Foreword ...............................................................................................................................7 Acknowledgments .................................................................................................................9 Welcome Remarks Richard Gilbrech ..........................................................................................................11 Steve Fisher ...................................................................................................................13 Chapter One - Robert Biggs, Rocketdyne - F-1 Saturn V First Stage Engine .......................15 -
“USC Engineering and I Grew up Together,” Viterbi Likes to Say
Published by the University of Southern California Volume 2 Issue 2 Let There Be Light A Revolution in BioMed Imaging Small and Deadly A Proper Name Searching for Air A Proper Name Pollution Solutions Viterbis Name School of Engineering Digital Reunion Reuniting the Parthenon and its Art Spring/Summer 2004 One man’s algorithm changed the way the world communicates. One couple’s generosity has the potential to do even more. Andrew J. Viterbi: Presenting The University of Southern California’s • Inventor of the Viterbi Algorithm, the basis of Andrew and Erna Viterbi School of Engineering. all of today’s cell phone communications • The co-founder of Qualcomm • Co-developer of CDMA cell phone technology More than 40 years ago, we believed in Andrew Viterbi and granted him a Ph.D. • Member of the National Academy of Engineering, the National Academy of Sciences and the Today, he clearly believes in us. He and his wife of nearly 45 years have offered American Academy of Arts and Sciences • Recipient of the Shannon Award, the Marconi Foundation Award, the Christopher Columbus us their name and the largest naming gift for any school of engineering in the country. With the Award and the IEEE Alexander Graham Bell Medal • USC Engineering Alumnus, Ph.D., 1962 invention of the Viterbi Algorithm, Andrew J. Viterbi made it possible for hundreds of millions of The USC Viterbi School of Engineering: • Ranked #8 in the country (#4 among private cell phone users to communicate simultaneously, without interference. With this generous gift, he universities) by U.S. News & World Report • Faculty includes 23 members of the National further elevates the status of this proud institution, known from this day forward as USC‘s Andrew Academy of Engineering, three winners of the Shannon Award and one co-winner of the 2003 Turing Award and Erna Viterbi School of Engineering. -
Rocketdyne R-6636-L FINAL RE PORT FLUORINE-HYDROGEN
(THRU) ° %/ / (PAGES) (CODE:) NASA CR-5497_ _-_ (NASA CR OR TMX OR AD NUMBER) (CATEGORY) Rocketdyne R-6636-l FINAL RE PORT FLUORINE-HYDROGEN PERFORMANCE EVALUATION .J PHASE I, PART I : ANALYSIS, DESIGN, AND DEMONSTRATION HIGH-PERFORMANCE INJECTORS FOR THE LIQUID F LUORINE- GASE OUS HYDROGEN PROPE L LANT C OMBINATION By GPO PRICE $ i{ H. A. Arbit CFSTI PRICE(S)•$ So Do Clapp Hard copy (HC) Microfiche (M F) ff 653 July 65 prepared for NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Contract NASw- 1229 ROCKETDYNE RESEARCH DEPARTMENT North American Aviation, Inc. 6633 Canoga Avenue, Canoga Park, California NOTI CE This report was prepared as an account of Government sponsored Work. Neither the United States, nor the National Aeronautics and Space Administration (NASA), nor any person acting on be- half of NASA: A.) Makes any warranty or representation, expressed or implied, with respect to the accuracy, completeness, or usefulness of the information contained in this report, or that the use of any information, apparatus, method, or process disclosed in this report may not infringe privately owned rights; or B.) Assumes any liabilities with respect to the use of, ¢ or for damages resulting from the use of any infor- mation, apparatus, method or process disclosed in this report. As used above, "person acting on behalf of NASA" includes any employee or contractor of NASA, or employee of such contractor, to the extent that such employee or contractor of NASA or employee of such contractor prepares, disseminates, or provides access to, any information pursuant to his employment or contractor with NASA, or his employment with such contractor.