NASA Facts Stennis @ 60

Total Page:16

File Type:pdf, Size:1020Kb

NASA Facts Stennis @ 60 National Aeronautics and Space Administration Stennis @ 60 60 Facts Spanning 60 Years facts Stennis conducts its first test of an RS-25 engine – to help power NASA’s Space Launch System rocket – on the A-1 Test Stand on Jan. 9, 2015. On Oct. 25, 2021, NASA’s Stennis Space Center marks the 60th anniversary of the agency’s NASA announcement to build a propulsion test site in south Mississippi. The following 60 fun facts offer a glimpse of the historic site that has powered the nation’s space dreams for six decades and counting. Historical Facts l NASA publicly announced plans to open a rocket l Tree-cutting for construction of test facilities at engine test facility in Hancock County in south Stennis began May 17, 1963. Mississippi on Oct. 25, 1961. l During construction at Stennis in the 1960s, some l Construction of Stennis Space Center facilities 6,100 employees were onsite with 30 prime and necessitated the relocation of 660 families. 250 subcontractor companies. l In an area meeting after NASA announced plans l Workers endured snakes, mosquito infestations, to build a test site in Mississippi, then-U.S. Sen. and inclement weather in constructing Stennis. John C. Stennis told a gathering of area residents, Category 4 Hurricane Betsy hit the Gulf Coast “There is always the thorn before the rose. ... You area on Sept. 10, 1965, but failed to derail the have got to make some sacrifices, but you will be building project, one of the largest underway in the taking part in greatness.” U.S. at the time. l Early on, rocket scientist Dr. Wernher von Braun affirmed the 30 percent of site employees reside in Louisiana, primarily in St. importance of Stennis by stating, “I don’t know yet what method Tammany Parish. we will use to get to the Moon, but I do know that we have to go l In 2012, Stennis partnered with a community foundation to open through Mississippi to get there!” nearby INFINITY Science Center. The 72,000-square-foot facility l NASA first named its propulsion test facility as Mississippi Test serves as the center’s official visitors center and features a mix Operations, then National Space Technology Laboratories. It was of exhibits and activities, allowing guests to explore Earth and designated Stennis Space Center by presidential proclamation on space through artifacts, tours, memorable experiences, educational May 20, 1988. programs, and citizen science opportunities. l In 2016, the Federal Aviation Administration expanded the Stennis Space Center restricted airspace at Stennis, enabling the site to perform l Stennis features a seven-and-a-half-mile canal network, which propulsion testing safely and allowing Stennis tenants to includes a lock system that effectively and efficiently allows transport of large conduct military exercises. rocket stages and cryogenic l NASA consistently ranks barges from the Gulf of as the best place to work in Mexico to on-site locations via the federal government, with the Pearl River. Stennis ranked at or near the l All Stennis facilities are top among the agency’s 10 located within a federal- individual centers. owned 13,800-acre “fee” area. The area is surrounded by a Propulsion Testing 125,000-acre acoustical buffer l Stennis is America’s largest zone, which is designated a rocket propulsion test site with national asset and allows for testing facilities valued at more large-scale test activities to be than $2 billion. conducted 365/24/7 without disturbing area residents and l NASA’s Rocket Propulsion businesses. Test Program Office is located at Stennis. The office is l In April 2008, the American responsible for managing test Institute of Aeronautics and assets, activities, and resources Astronautics named Stennis a across the agency. historic aerospace site. l The three original test stands l Stennis has been affected at Stennis are the single- by numerous tropical storm position, vertical-firing A-1 systems through its 60 years, Test Stand and A-2 Test Stand, including several major and the dual-position, vertical- hurricanes – Betsy (1965), firing B-1/B-2 Test Stand. Camille (1969), Katrina (2005) l and Zeta (2020). In 2007, Stennis broke ground for construction of the A young INFINITY Science Center visitor dreams of a space future. l Stennis serves as a major A-3 Test Stand, the first large economic engine for the test facility to be built on site Gulf Coast region. In 2020, the direct global economic impact of since construction of the original test stands in the 1960s. Stennis was $877.9 million. The direct economic impact within a l 50-mile radius of the facility was $656.6 million. The A-3 Test Stand at Stennis is the only stand in the country with the combined capabilities to conduct long-duration tests l A national center for research, military logistics, and applied on full-scale engines at simulated altitudes up to 100,000 feet, science, in 2020, Stennis spent almost 74 cents of every dollar and to gimbal, or pivot, the engines during testing as they must within a 50-mile radius from the center. operate in flight. l More than half of all Stennis employees (52 percent) hold a l A versatile E Test Complex at Stennis includes seven separate cells bachelor’s degree or greater. capable of various component, engine, and stage test activities. l Sixty-two percent of Stennis employees live in three surrounding l Stennis is among the world’s largest consumers of liquid hydrogen Mississippi counties – Hancock, Harrison and Pearl River. About – one of the primary fuels used in rocket propulsion testing. Apollo Program Space Launch System / Artemis Program l First and second Saturn V rocket stages for NASA’s Apollo l Stennis remains at the forefront of America’s space programs, Program were tested at Stennis, including those that propelled testing rocket stages and engines for NASA’s Space Launch humans to the Moon on seven lunar missions from 1969 to 1972. System rocket that will carry humans back to the Moon and, eventually, to Mars. l Stennis operators conducted the first-ever rocket engine test at the site on April 23, 1966, a 15-second firing of a Saturn V second l NASA’s Space Launch System will be powered at launch, in part, stage prototype (S-II-C). by four RS-25 engines. Stennis conducted the first RS-25 engine test on Jan. 9, 2015, and will test all RS-25 engines for the rocket. l During the Apollo Program years, Stennis engineers conducted 43 test firings. The accumulated experience of the test team members l Stennis is conducting both developmental and flight hardware amounted to 2,475 man-years of rocket engine test expertise. testing for RS-25 engines on the historic A-1 Test Stand. This includes testing of new cutting-edge flight components, such as l The Stennis team tested 27 3D-printed parts. Saturn V rocket stages in the Apollo years. All of the stages l A hot fire on April 4, 2019, that were launched performed concluded 51 months of their designated missions RS-25 testing on the A-1 Test without a single failure. Stand for Phase 1 of the RS- 25 engine restart program and Space Shuttle Program completed acceptance testing of all 16 engines that will help l Stennis operators conducted launch the first four Space the first full-duration test of Launch System missions. a space shuttle main engine on June 24, 1975. The center l Green Run testing of the first went on to test all main Space Launch System core engines used to launch 135 stage was conducted on the shuttle flights from 1981 to B-2 Test Stand in 2020 and 2011. Stennis conducted its early 2021. The test series last test of a space shuttle marked the first time the new main engine on the A-2 Test core stage had been fully Stand on July 29, 2009. powered up and culminated with a hot fire of its four l In April 1978, Stennis RS-25 engines, just as during a conducted the first test of the launch. Following Green Run, space shuttle main propulsion the core stage was delivered test article with three main to Kennedy Space Center for engines configured as they use on the maiden Artemis I are on a shuttle orbiter during mission. flight. All three were fired simultaneously on the B-2 Test l Stennis is preparing to test the Stand to prove the propulsion Exploration Upper Stage for NASA’s Space Launch System system flightworthy. An A-1 Test Stand camera offers close-up view of RS-25 hot fire. rocket. The Green Run testing l All modifications and of the new rocket stage is configurations of space shuttle main engines were tested and scheduled to be conducted on the B-2 Test Stand. proven flightworthy at Stennis before being flown on a mission. Partnership Testing l Space shuttle main engines at Stennis were test fired for 520 l seconds (more than eight minutes), the same time the engines fire In 1998, Stennis partnered with Aerojet Rocketdyne to test RS-68 during an actual flight to enable the shuttle to reach orbit. engines used for Delta IV rocket launches. It marked the first longterm commitment to allow Stennis test facilities to be used l On Aug. 20, 1990, for the first time, space shuttle main engines for commercial purposes. were tested on all three large test stands at Stennis in a single day. l Stennis has worked with multiple commercial test partners to l The 1 millionth second of space shuttle main engine test firing test engines and components needed for their individual space was recorded at Stennis on Jan.
Recommended publications
  • Constellation Program Overview
    Constellation Program Overview October 2008 hris Culbert anager, Lunar Surface Systems Project Office ASA/Johnson Space Center Constellation Program EarthEarth DepartureDeparture OrionOrion -- StageStage CrewCrew ExplorationExploration VehicleVehicle AresAres VV -- HeavyHeavy LiftLift LaunchLaunch VehicleVehicle AltairAltair LunarLunar LanderLander AresAres II -- CrewCrew LaunchLaunch VehicleVehicle Lunar Capabilities Concept Review EstablishedEstablished Lunar Lunar Transportation Transportation EstablishEstablish Lunar Lunar Surface SurfaceArchitecturesArchitectures ArchitectureArchitecture Point Point of of Departure: Departure: StrategiesStrategies which: which: Satisfy NASA NGO’s to acceptable degree ProvidesProvides crew crew & & cargo cargo delivery delivery to to & & from from the the Satisfy NASA NGO’s to acceptable degree within acceptable schedule moonmoon within acceptable schedule Are consistent with capacity and capabilities ProvidesProvides capacity capacity and and ca capabilitiespabilities consistent consistent Are consistent with capacity and capabilities withwith candidate candidate surface surface architectures architectures ofof the the transportation transportation systems systems ProvidesProvides sufficient sufficient performance performance margins margins IncludeInclude set set of of options options fo for rvarious various prioritizations prioritizations of cost, schedule & risk RemainsRemains within within programmatic programmatic constraints constraints of cost, schedule & risk ResultsResults in in acceptable
    [Show full text]
  • Silencing Nasa's Space Shuttle Crawler
    SILENCING NASA’S SPACE SHUTTLE CRAWLER TRANSPORTER R. MacDonalda, C. Faszerb, and R. Margasahayamc aNoise Solutions Inc., #310 605 – 1st Street SW, Calgary, Alberta, Canada T2P 3S9 bFaszer Farquharson & Associates, #304 605 – 1st Street SW, Calgary, Alberta, Canada T2P 3S9 cNASA, John F. Kennedy Space Center, Florida, United States of America 32899 [email protected]; [email protected]; [email protected] Abstract. The crawler transporter (CT) is the world’s second largest known tracked vehicle, weighing 6 million pounds with a length of 131 feet and a width of 113 feet. The Kennedy Space Center (KSC) has two CTs that were designed and built for the Apollo program in the 1960’s, maintained and retrofitted for use in the Space Shuttle program. As a key element of the Space Shuttle ground systems, the crawler transports the entire 12-million-pound stack comprising the orbiter, the mobile launch platform (MLP), the external tank (ET), and the solid rocket boosters (SRB) from the Vehicle Assembly Building (VAB) to the launch pad. This rollout, constituting a 3.5 to 5.0 mile journey at a top speed of 0.9 miles-per-hour, requires over 8 hours to reach either Launch Complex 39A or B. This activity is only a prelude to the spectacle of sound and fury of the Space Shuttle launch to orbit in less than 10 minutes and traveling at orbital velocities of Mach 24. This paper summarizes preliminary results from the Crawler Transporter Sound Attenuation Study, encompassing test and engineering analysis of significant sound sources to measure and record full frequency spectrum and intensity of the various noise sources and to analyze the potential for noise mitigation.
    [Show full text]
  • Handout – Innovative Business Agreements and Related Cost
    MG-4 - Innovative Business Agreements and Related Cost & Pricing Methods at NASA in Support of New Commercial Programs Kennedy Space Center - CFO Business & Cost Assessment Office Innovative Business Agreements and Related Cost & Pricing Methods at NASA in Support of New Commercial Programs JIM ROBERTS & TERRY LAMBING NASA Kennedy Space Center Office of the CFO ICEAA National Conference June 2014 Kennedy Space Center - CFO Business & Cost Assessment Office Background.. • Immediately after Shuttle retirement decision in 2004, transition planning for NASA’s facilities was begun. • In April 2010 President Obama delivered a speech at Kennedy Space Center in which he outlined his new vision for the U.S. space program. Emphasis was placed on enabling the exploration of Space by Commercial entities instead of by Government. • The Constellation Program - which was to fill the void of the retiring Space Shuttle Program - was cancelled. • Facilities no longer needed for remaining NASA programs were identified, and NASA Centers were charged with leveraging value of underutilized property through initiatives such as out-leasing. • Focus was placed on development of Commercial Business Partnerships to enable commercial space activities using unused or available facilities and launch infrastructure. 5/23/2014 2 1 ICEAA 2014 Professional Development & Training Workshop MG-4 - Innovative Business Agreements and Related Cost & Pricing Methods at NASA in Support of New Commercial Programs Kennedy Space Center - CFO Business & Cost Assessment Office Kennedy
    [Show full text]
  • NASA Begins Engine Test Project for Space Launch System Rocket 21 July 2014, by Rachel Kraft
    NASA begins engine test project for space launch system rocket 21 July 2014, by Rachel Kraft shuttle," said Steve Wofford, SLS Liquid Engines Element manager. "This testing will confirm the RS-25 will be successful at powering SLS." Early tests on the engine will collect data on the performance of its new advanced engine controller and other modifications. The controller regulates valves that direct the flow of propellant to the engine, which determines the amount of thrust generated during an engine test, known as a hotfire test. In flight, propellant flow and engine thrust determine the speed and trajectory of a spacecraft. The controller also regulates the engine startup sequence, which is especially important on an engine as sophisticated as the RS-25. Likewise, the controller determines the engine shutdown sequence, ensuring it will proceed properly under RS-25 rocket engine No. 0525 is positioned onto the A-1 both normal and emergency conditions. Test Stand at NASA’s Stennis Space Center in Mississippi in preparation for a series of developmental "Installation of RS-25 engine No. 0525 signals the tests. Credit: NASA launch of another major rocket engine test project for human space exploration on the A-1 Test Stand," said Gary Benton, RS-25 rocket engine test project manager at Stennis. (Phys.org) —Engineers have taken a crucial step in preparing to test parts of NASA's Space Launch The SLS is designed to carry astronauts in NASA's System (SLS) rocket that will send humans to new Orion spacecraft deeper into space than ever destinations in the solar system.
    [Show full text]
  • NASA's Space Launch System
    https://ntrs.nasa.gov/search.jsp?R=20160006989 2019-08-31T02:36:41+00:00Z View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by NASA Technical Reports Server SP2016_AP2 NASA’s Space Launch System: An Evolving Capability for Exploration Stephen D. Creech(1), Dr. Kimberly F. Robinson(2) (1)Deputy Manager , SLS Spacecraft/Payload Integration and Evolution, XP50, NASA Marshall Space Flight Center, Alabama, 35812, USA, [email protected] (2)SLS Strategic Communications Manager, XP02, NASA Marshall Space Flight Center, Alabama, 35812, USA, [email protected] ABSTRACT: launch capability via an affordable and sustainable development path. Designed to meet the stringent requirements of human exploration missions into deep space and to Mars, NASA’s Space Launch System (SLS) vehicle represents a unique new launch capability opening new opportunities for mission design. NASA is working to identify new ways to use SLS to enable new missions or mission profiles. In its initial Block 1 configuration, capable of launching 70 metric tons (t) to low Earth orbit (LEO), SLS is capable of not only propelling the Orion crew vehicle into cislunar space, but also delivering small satellites to deep space destinations. The evolved configurations of SLS, including both the 105 t Block 1B and the 130 t Block 2, offer opportunities for launching co-manifested payloads and a new class of secondary payloads with the Orion crew vehicle, and also offer the capability to carry 8.4- or 10-m payload fairings, larger than any contemporary launch vehicle, delivering unmatched mass-lift capability, payload volume, and C3.
    [Show full text]
  • Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC
    DOCUMENT RESUME ED 312 131 SE 050 900 AUTHOR Morrison, David; Samz, Jane TITLE Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC. Scientific and Technical Information Branch. REPORT NO NASA-SP-439 PUB DATE 80 NOTE 208p.; Colored photographs and drawings may not reproduce well. AVAILABLE FROMSuperintendent of Documents, U.S. Government Printing Office, Washington, DC 20402 ($9.00). PUB TYPE Reports - Descriptive (141) EDRS PRICE MF01/PC09 Plus Postage. DESCRIPTORS Aerospace Technology; *Astronomy; Satellites (Aerospace); Science Materials; *Science Programs; *Scientific Research; Scientists; *Space Exploration; *Space Sciences IDENTIFIERS *Jupiter; National Aeronautics and Space Administration; *Voyager Mission ABSTRACT This publication illustrates the features of Jupiter and its family of satellites pictured by the Pioneer and the Voyager missions. Chapters included are:(1) "The Jovian System" (describing the history of astronomy);(2) "Pioneers to Jupiter" (outlining the Pioneer Mission); (3) "The Voyager Mission"; (4) "Science and Scientsts" (listing 11 science investigations and the scientists in the Voyager Mission);.(5) "The Voyage to Jupiter--Cetting There" (describing the launch and encounter phase);(6) 'The First Encounter" (showing pictures of Io and Callisto); (7) "The Second Encounter: More Surprises from the 'Land' of the Giant" (including pictures of Ganymede and Europa); (8) "Jupiter--King of the Planets" (describing the weather, magnetosphere, and rings of Jupiter); (9) "Four New Worlds" (discussing the nature of the four satellites); and (10) "Return to Jupiter" (providing future plans for Jupiter exploration). Pictorial maps of the Galilean satellites, a list of Voyager science teams, and a list of the Voyager management team are appended. Eight technical and 12 non-technical references are provided as additional readings.
    [Show full text]
  • The First Human Asteroid Mission: Target Selection and Conceptual Mission Design
    The First Human Asteroid Mission: Target Selection and Conceptual Mission Design Daniel Zimmerman,∗ Sam Wagner,∗ and Bong Wiey Asteroid Deflection Research Center - Iowa State University, Ames, IA 50011-2271 President Obama has recently declared that NASA will pursue a crewed mission to an asteroid by 2025. This paper identifies the optimum target candidates of near-Earth objects (NEOs) for a first crewed mission between 2018 and 2030. Target asteroids in the NEO database with orbital elements that meet predetermined requirements are analyzed for mission design. System architectures are then proposed to meet the require- ments for five designated NEO candidates. Additional technology which can be applied to crewed NEO mis- sions in the future is also discussed, and a previous NEO target selection study is analyzed. Although some development of heavy launch vehicles is still required for the first NEO mission, design examples show that a first mission can be achieved by 2025. The Ares V and the Orion CEV are used as the baseline system architecture for this study. Nomenclature a Semi-major Axis (AU) AU Astronomical Unit BOM Burnout Mass CEV Crew Exploration Vehicle e Eccentricity EDS Earth Departure Stage EOR Earth Orbit Rendezvous H Absolute Magnitude i Inclination (deg) Isp Specific Impulse (s) ISS International Space Station JPL Jet Propulsion Laboratory LEO Low-Earth Orbit LH2 Liquid Hydrogen LOX Liquid Oxygen MWe Megawatt Electrical MT Metric Ton NASA National Aeronautics and Space Administration NEO Near-Earth Object OT V Orbital Transfer Vehicle RSRM Reusable Solid Rocket Motor SSME Space Shuttle Main Engine T LI Trans Lunar Injection V ASIMR Variable Specific Impulse Magnetoplasma Rocket ∆V Velocity Change (km/s) ∗Graduate Research Assistant, Dept.
    [Show full text]
  • NASA's Space Launch System Capabilities for Ultra-High C3
    Heliophysics 2050 White Papers (2021) 4057.pdf NASA’s Space Launch System Capabilities for Ultra-High C3 Missions A White Paper for the Heliophysics Survey Robert W. Stough, James B. Holt, Dr. Kimberly F. Robinson, David A. Smith, W. David Hitt, Beverly A. Perry NASA’s Marshall Space Flight Center Dr. Ralph L. McNutt Jr., Michael V. Paul Johns Hopkins University Applied Physics Laboratory 1. Executive Summary Designed to meet NASA’s requirements for human exploration of the Moon, Mars and beyond, the Space Launch System (SLS) vehicle offers enhancing and enabling capabilities for a variety of missions. Using commercially available propulsion systems as third and/or fourth stages, SLS offers C3 performance double the highest-C3 missions ever flown. This capability can be game- changing for missions into the interstellar medium or for high-energy solar observation missions. Today, SLS is making progress toward its initial launch capability and toward both future launches and future capabilities. In addition, NASA has issued contracts with prime contractors for SLS hardware for delivery well into the 2030s. 2. Overview The initial configuration of SLS, the Block 1 crew vehicle, is powered at launch by four RS-25 engines and two solid rocket boosters, with an almost 67 meter (m) tall core stage. In-space propulsion is provided by an interim cryogenic propulsion stage (ICPS). The Block 1 vehicle can be flown in a cargo configuration utilizing a commercially available 5 m fairing. The next configuration of SLS, Block 1B, upgrades the upper stage to an exploration upper stage (EUS) equipped with four RL10s.
    [Show full text]
  • Kennedy Space Center Overview Kennedy Space Center
    National Aeronautics and Space Administration Kennedy Space Center Overview Kennedy Space Center fter five decades, NASA’s John F. AKennedy Space Center continues to set the stage for America’s adventure to space. Kennedy Space Center shares a boundary with the Merritt Island National Wildlife Refuge on Florida’s east coast, where nature and technology co-exist. The refuge includes about 140,000 acres on land and water and provides a wide variety of habitats, including coastal dunes, saltwater estuaries and marshes, facts freshwater impoundments, scrub, pine flatwoods, and hardwood hammocks that provide habitat for more than 1,500 species of plants and animals. Kennedy Space Center offers 6,000 acres of land for facilities and roads, and has 7.8 million square feet of building area, and 564 miles of roads, including 184 miles of paved and 380 miles of unpaved roads. The combined spaceport (Kennedy and Cape Canaveral Air Telescope to the Mars exploration rovers, nedy will continue to support International Force Station (CCAFS)) has served as Kennedy enjoys a rich heritage in its vital Space Station operations as the orbiting the departure gate for every American role as NASA’s processing and launch laboratory enters its second decade of human space mission and for hundreds center. discoveries. And NASA’s Launch Servic- of rocket launches carrying advanced As NASA transitions from the Space es Program managed at Kennedy Space NASA research and interplanetary spacecraft. Shuttle Program to future endeavors, Center will continue to launch satellites From the early days of Project Mercury Kennedy’s work force remains focused and robotic missions on journeys to learn to the space shuttle and International on the agency’s core values: safety, more about our home planet and unlock integrity, teamwork, and excellence.
    [Show full text]
  • Ares V and RS-68B
    https://ntrs.nasa.gov/search.jsp?R=20090014109 2019-08-30T06:39:32+00:00Z Ares V and RS-68B Steve Creech, NASA MSFC Jim Taylor, NASA MSFC Lt. Col. Scott Bellamy, AFSPC Fritz Kuck, Pratt & Whitney Rocketdyne JANNAF Liquid Propulsion Subcommittee (LPS) JANNAF LPS Technical Steering Group RS-68/-68A/-68B Specialist Session 8-12 December 2008 Orlando, Florida ARES V and RS-68B Abstract Ares V is the heavy lift vehicle NASA is designing for 05 06 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25… lunar and other space missions. It has significantly more ExplorationExploration andand ScienceScience LunarLunar RoboticsRobotics MissionsMissions LunarLunar OutpostOutpost BuildupBuildup lift capability than the Saturn V vehicle used for the Research and Technology DevelopmentDevelopment on ISS Apollo missions to the moon. Ares V is powered by two Commercial Orbital Transportation Services for ISS recoverable 5.5 segment solid rocket boosters and six RS-68B engines on the core stage. The upper stage, SpaceSpace ShuttleShuttle OperationsOperations SSPSSP TransitionTransition designated as the Earth Departure Stage, is powered by a Ares I and OrionOrion Development Operations CapabilityCapability Development single J-2X engine. This paper provides an overview of (EVA(EVA Systems,Systems, GroundGround Operations,Operations, MissionMission Operations)Operations) Ares I-X Orion andand Ares I Production andand Operation Test Flight the Ares V vehicle and the RS-68B engine, an upgrade April 2009 to the Pratt & Whitney Rocketdyne RS-68 engine Altair Development developed for the Delta IV vehicle. Ares VV && EarthEarth Departure Stage SurfaceSurface SystemsSystems DevelopmentDevelopment 032408 Constellation Program Figure 2.
    [Show full text]
  • Aerojet Rocketdyne Completes J-2X Testing
    June 26, 2014 Aerojet Rocketdyne Completes J-2X Testing SACRAMENTO, Calif., June 26, 2014 (GLOBE NEWSWIRE) -- Aerojet Rocketdyne, a GenCorp (NYSE:GY) company, recently completed its final J-2X test series at NASA's Marshall Space Flight Center. Over a period of three years, Aerojet Rocketdyne teams manufactured, assembled and tested four newly developed engine test articles that achieved an accumulated duration of nearly five hours firing time and demonstrated full power operation for twice its designed life service. Delivering 30 percent more thrust and five percent more performance than the J-2 Apollo-era engine, upon which it is based, the J-2X is the highest performing human-rated upper-stage engine to be developed in nearly 40 years. "With J-2X, we were able to drive down the time needed to take a new rocket engine to 100 percent power level in testing, from 651 days to just 29, by integrating modern design, analysis and test practices with decades of experience gained on multiple engine development programs," said Aerojet Rocketdyne President Warren M. Boley, Jr. "That kind of knowledge isn't retained anywhere else in the industry and it demonstrates that we know how to design an engine that will work the first time." The J-2X is a liquid-oxygen/liquid-hydrogen fueled engine that is designed to start at altitude and re-start in space as part of a second or third stage of a large, multi-stage launch vehicle. With its full nozzle extension installed, the J-2X measures more than 15 feet tall and 10 feet in diameter at its base and weighs approximately 5,400 pounds.
    [Show full text]
  • Subcommittee on Space and Aeronautics Committee on Science, Space, and Technology U.S. House of Representatives Hearing Charter
    SUBCOMMITTEE ON SPACE AND AERONAUTICS COMMITTEE ON SCIENCE, SPACE, AND TECHNOLOGY U.S. HOUSE OF REPRESENTATIVES HEARING CHARTER Developing Core Capabilities for Deep Space Exploration: An Update on NASA’s SLS, Orion, and Exploration Ground Systems Programs Wednesday, September 18, 2019 10:00 a.m. 2318 Rayburn House Office Building PURPOSE The purpose of the hearing is to assess the status, including the progress, challenges, and other issues, of NASA’s Exploration Systems Development programs (the Space Launch System, Orion Multipurpose Crew Vehicle, and Exploration Ground Systems). WITNESSES • Mr. Kenneth Bowersox, Associate Administrator (Acting), Human Exploration and Operations, National Aeronautics and Space Administration • Ms. Cristina Chaplain, Director, Contracting and National Security Acquisitions, U.S. Government Accountability Office • Mr. Doug Cooke, Owner, Cooke Concepts and Solutions; Former Associate Administrator, Exploration Systems, National Aeronautics and Space Administration OVERARCHING QUESTIONS • What are current challenges and upcoming milestones for the Space Launch System (SLS), Orion, and Exploration Ground Systems (EGS) programs? • What are the biggest drivers of cost growth and schedule challenges for the SLS, Orion, and EGS programs? • How can Congress best ensure that schedule pressure does not compromise safety in the SLS, Orion, and EGS programs? • What are NASA’s plans for SLS and Orion after sending humans to the Moon in 2024? BACKGROUND NASA is developing a new heavy-lift rocket and crew vehicle capable of returning humans to deep space—generally defined as anywhere beyond low Earth orbit (LEO), about 1,200 miles above the Earth’s surface—for the first time since the last Apollo astronauts landed on the Moon 1 in 1972.
    [Show full text]