RS-25 for NASA's Space Launch System
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AEROJET ROCKETDYNE PROPRIETARY 0 THIS DOCUMENT CONTAINS NO EXPORT CONTROLLED – ITAR/USML CATEGORY IV September 2016 Aerojet Rocketdyne Footprint International Offices: Redmond, WA Moscow Tokyo London Belfast UAE Picatinny Arsenal, NJ Sacramento, CA Clearfield, UT ARDÉ, NJ Headquarters Washington, D.C. Denver, CO Gainesville, VA Orange, VA Los Angeles, CA Jonesboro, TN Vernon, CA Camden, AR Socorro, NM Tucson, AZ Huntsville, AL Headquarters Dallas, TX Orlando, FL Operating Locations Stennis, MS Eglin AFB, FL Field Offices West Palm Beach, FL Nearly 5,000 Employees Across 14 States 140 and Growing at NASA Stennis Space Center Aerojet Rocketdyne Proprietary 1 Aerojet Rocketdyne & NASA Stennis Space Center (SSC): A Fifty Year Partnership • NASA-SSC is the nation’s Center of Excellence for large space transportation propulsion systems testing • Tested each of the F-1 rocket engines that powered the first stage of the Saturn V launch vehicle for the Apollo missions • Early 1970s, SSC’s facilities were modified to test the space shuttle's main engines (SSMEs) • All the 405 flown engines supporting 135 shuttle flights tested and proven flight-worthy at SSC • SSC’s state-of-the-art facilities continues to assemble and test components and engines for future Space Launch System (SLS) missions (RS-25 and J-2X) • RS-68/A engines supporting the Delta IV program launching national security satellites and recently the Orion Capsule for NASA’s Exploration Flight Test-1 Aerojet Rocketdyne Proprietary 2 SSC Facilities Occupied by Aerojet Rocketdyne • A1 Test Stand– RS-25 (1st Stage booster for SLS) • Primary Customer – NASA • Aerojet Rocketdyne Test Article Contractor • B Test Stand • B1 - RS-68 (1st Stage booster for Delta-IV) • Primary Customer – Air Force (ULA) • Test Stand is operated under a Space Act Agreement • B2 (RS-25 Space Launch System Stage Testing) • B Complex Test Control Center (BTCC) • Engine Assembly Facility (EAF – Bldg. 9101) • Leased Facility from NASA via Space Act Agreement • 40,000 sf Assembly Space • 100,000 sf Warehouse / Office Space • Key Capabilities • Assembly of Large Rocket Engines (RS-25, RS-68A) • Development and Flight Certification Testing • Warehouse, Store and Ship Flight & Development Engines and Associated Hardware Aerojet Rocketdyne Proprietary 3 Aerojet Rocketdyne at Stennis Current Activities . Large Liquid Rocket Engine Final Assembly and Testing RS-25 o RS-25 for NASA’s Space Launch System (SLS) o RS-68 for ULA’s Delta IV Launch Vehicle Future Activities RS-68 . Final Assembly and Testing of AR1 Launch Engine o Advanced Kerosene Engine to replace the Russian RD-180 on National Security Space Launch missions AR-1 Aerojet Rocketdyne Proprietary 4 Current Activities -- RS-25 Hot Fire Testing • RS-25 – Slated to serve as core propulsion of NASA’s Space Launch System (SLS) • Four engines per SLS Rocket – Upgraded version of the Space Shuttle Main Engine (SSME) • 100% Mission Success on Space Shuttle Program – Fueled by Liquid Oxygen/Hydrogen – Staged Combustion – Approximately 500,000 lbs of thrust RS-25 – Testing began in Jan 2009 Core Engine for SLS – Maintaining Affordability is Paramount 5 Aerojet Rocketdyne Proprietary 7,300 PSI Pressures equal to 3 miles under the ocean -423° F 2nd coldest fluid on Earth 6,000° F Hotter than boiling iron 35,000 RPM Turbopumps rotating 580 times per second THE RS-25: STATE OF THE ART PROPULSION FOR THE WORLD’S MOST POWERFUL ROCKET RS-25 Engine Four RS-25 Engines Current Activities -- Hot Fire Testing of RS-68 RS-68 1st Stage Booster: Launch of ULA’s Delta IV • Powers ULA’s Delta IV Heavy Rocket Rocket • Powered by three RS-68 • Liquid Oxygen/Liquid Boost Engines Hydrogen Fuel • Over 700,000 pounds of thrust 8 Aerojet Rocketdyne Proprietary Propulsion on All ULA Launch Vehicles • Primary propulsion provider to ULA Launch System Solution every ULA launch vehicle: Delta II, Delta IV and Atlas V • AR supplies boost main engines, upper stage main engines, upper stage RCS, solid strap-on motors • 100% mission success in >100 ULA launches to date • Cost reduction initiatives • Delivering the nation’s most important security and civil payloads The Nation’s Leading Provider of Every Type Of Space Launch Propulsion Aerojet Rocketdyne Proprietary 9 Component Testing in the E Complex Full power level test of 40k Overhead Support Trolley preburner System (OSTS) System is used to support component change out LOX inlet piping for FSPB This document contains no ITAR or EAR controlled technical information Aerojet Rocketdyne10 Proprietary AR1 Baseline Production Plan is Based on 10 Flights/Year 20 Engines/ Year and Integration of 10 MPS Component Fabrication Procurement, & Assembly Engine Hot-Fire Test (AR-LA, Sacramento, WPB & Supplier (Mississippi - NASA SSC) Locations) Vehicle Ass’y & Launch Ops (CCAFS or VAFB) Engine Assembly (Mississippi - NASA SSC) Booster Stage Integration This document contains no ITAR or EAR controlled technical information Aerojet Rocketdyne Proprietary 11 Facility Layout Development • Refining 9101 Facility Layout through requirements definition, modeling/simulations, IMS development and three phase 3P Process This document contains no ITAR or EAR controlled technical information Aerojet Rocketdyne Proprietary Assembly Facility Modeling This document contains no ITAR or EAR controlled technical information Aerojet Rocketdyne13 Proprietary AR1 Program Status Assembly Facility Modeling (Pneumatic Panels) This document contains no ITAR or EAR controlled technical information Aerojet Rocketdyne14 Proprietary AR1 Program Status Assembly Facility Modeling (Kit Staging) This document contains no ITAR or EAR controlled technical information Aerojet Rocketdyne15 Proprietary AR1 Program Status Questions? 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