Upper Stage Evolution

Similar documents
July 28, ULA Rideshare Capabilities

2012 Cubesat Workshop. ULA Rideshare Update APR 19, 2012

ULA Briefing to National Research Council. In-Space Propulsion Roadmap. March 22, Bernard Kutter. Manager Advanced Programs. File no.

United Launch Alliance Rideshare Capabilities To Support Low-Cost Planetary Missions

The GHOST of a Chance for SmallSat s (GH2 Orbital Space Transfer) Vehicle

Abstract. 1 American Institute of Aeronautics and Astronautics

Space Transportation Atlas V / Auxiliary Payload Overview

The DoD Space Test Program Standard Interface Vehicle (ESPA) Class Program

Atlas V Launches the Orbital Test Vehicle-1 Mission Overview. Atlas V 501 Cape Canaveral Air Force Station, FL Space Launch Complex 41

Current Launch System Industrial Base

MISSION OVERVIEW SLC-41 CCAFS, FL

Abstract #1754. English. French. Author(s) and Co Author(s) Resources in the cislunar marketplace. To follow. No abstract title in French

On Orbit Refueling: Supporting a Robust Cislunar Space Economy

MISSION OVERVIEW SLC-41

SPACE LAUNCH SYSTEM. Steve Creech Manager Spacecraft/Payload Integration & Evolution August 29, 2017 A NEW CAPABILITY FOR DISCOVERY

Boeing CST-100. Commercial Crew Transportation System. Keith Reiley, The Boeing Company. February, 2011

Taurus II. Development Status of a Medium-Class Launch Vehicle for ISS Cargo and Satellite Delivery

Paper Session II-A - Lockheed Martin's Next Generation Launch Systems

ULA Rideshare with CubeSat Missions for Lunar & Inter-Planetary Exploration

Rocket 101. IPSL Space Policy & Law Course. Andrew Ratcliffe. Head of Launch Systems Chief Engineers Team

United Launch Alliance Rideshare Capabilities for Providing Low-Cost Access to Space

Lunar Surface Access from Earth-Moon L1/L2 A novel lander design and study of alternative solutions

Lunar Cargo Capability with VASIMR Propulsion

Ares I Overview. Phil Sumrall Advanced Planning Manager Ares Projects NASA MSFC. Masters Forum May 14, 2009

Ares V: Supporting Space Exploration from LEO to Beyond

SPACE PROPULSION SIZING PROGRAM (SPSP)

Cygnus Payload Accommodations: Supporting ISS Utilization

Cal Poly CubeSat Workshop 2014

Suborbital Flight Opportunities for Cubesat-Class Experiments Aboard NLV Test Flights

Lunette: A Global Network of Small Lunar Landers

Routine Scheduled Space Access For Secondary Payloads

Moon Express Summary. Dr. Andrew Aldrin President, Moon Express, Inc. 12 June, Science Network. Sample Return ME-1: GLXP

Leading the Way to Electric Propulsion in Belfast

The European Lunar Lander Mission

LAUNCHERONE: REVOLUTIONARY ORBITAL TRANSPORT FOR SMALL SATELLITES

The Common Spacecraft Bus and Lunar Commercialization

United Launch Alliance Update to Huntsville and Decatur-Morgan Chambers of Commerce

Solar Electric Propulsion Benefits for NASA and On-Orbit Satellite Servicing

Access to Space. ISRO s Current Launch. & Commercial Opportunities. S Somanath Project Director, GSLV Mk III VSSC, ISRO

A LEO Propellant Depot System Concept for Outgoing Exploration

A Model-Based Systems Engineering Approach to the Heavy Lift Launch System Architecture Study

Suitability of reusability for a Lunar re-supply system

QinetiQ Electric Propulsion

Copyright 2016 Boeing. All rights reserved.

Space Architecture. Master s Thesis Project Jain, Abhishek Dec. 2 nd, 2013

Dual Spacecraft System

MISSION OVERVIEW SLC-41

Enhanced. Chapter 3. Baseline

THE FALCON I LAUNCH VEHICLE Making Access to Space More Affordable, Reliable and Pleasant

AMSAT-NA FOX Satellite Program

ENERGIA 1. IDENTIFICATION. 1.1 Name. 1.2 Classification Family : K Series : K-1/SL-17 Version : 4 strap-ons

GK L A U N C H SER VICES MOSCOW 2017

CHAPTER 2 GENERAL DESCRIPTION TO LM-3C

Capabilities Summary and Approach to Rideshare for 20 th Annual Small Payload Rideshare Symposium NASA Ames Research Center June 12-14, 2018

Architecture Options for Propellant Resupply of Lunar Exploration Elements

NASA s Choice to Resupply the Space Station

Modular Reconfigurable Spacecraft Small Rocket/Spacecraft Technology Platform SMART

NanoRacks External Payload Platform

SABRE FOR HYPERSONIC & SPACE ACCESS PLATFORMS

FlexCore Low-Cost Attitude Determination and Control Enabling High-Performance Small Spacecraft

Thinking Outside the Cube

Massachusetts Space Grant Consortium

AMBR* Engine for Science Missions

The 1 N HPGP thruster is designed for attitude and orbit control of small-sized satellites. FLIGHT-PROVEN.

lights on, down 2 ½ 40 feet, down 2 ½ Kickin up some dust 30 feet, 2 ½ down faint shadow

Atlas V MSL. Mission Overview Cape Canaveral Air Force Station, FL

Fly Me To The Moon On An SLS Block II

EPIC Workshop 2017 SES Perspective on Electric Propulsion

EPIC Gap analysis and results

European Lunar Lander: System Engineering Approach

AN OPTIMIZED PROPULSION SYSTEM FOR Soyuz/ST

The SHuttle Expendable Rocket for Payload Augmentation (SHERPA)

SmallSats mission opportunities for the Vega launch system: the Small Spacecraft Mission Service 7 th August, 2016

RDT&E BUDGET ITEM JUSTIFICATION SHEET (R-2 Exhibit) June 2001

Development of a Low Cost Suborbital Rocket for Small Satellite Testing and In-Space Experiments

Blue Origin Achievements and plans for the future

Vehicle Reusability. e concept e promise e price When does it make sense? MARYLAND U N I V E R S I T Y O F. Vehicle Reusability

BIMODAL NUCLEAR THERMAL ROCKET (BNTR) PROPULSION FOR FUTURE HUMAN MARS EXPLORATION MISSIONS

BIMODAL NUCLEAR THERMAL ROCKET (BNTR) PROPULSION FOR FUTURE HUMAN MARS EXPLORATION MISSIONS

ReachMars 2024 A Candidate Large-Scale Technology Demonstration Mission as a Precursor to Human Mars Exploration

ORBITAL EXPRESS Space Operations Architecture Program 17 th Annual AIAA/USU Conference on Small Satellites August 12, 2003

INTERNATIONAL LUNAR NETWORK ANCHOR NODES AND ROBOTIC LUNAR LANDER PROJECT UPDATE

VACCO ChEMS. Micro Propulsion Systems

HYDROS Development of a CubeSat Water Electrolysis Propulsion System

Lunar Architecture and LRO

CHAPTER 1 INTRODUCTION

OLEV AN ON-ORBIT SERVICING PROGRAM FOR COMMERCIAL SPACECRAFTS IN GEO

ULA's new Vulcan rocket 24 June 2015, by Ken Kremer, Universe Today

The World Space Congress 2002, IAF - COSPAR October, 2002 Houston, Texas

SmallSats, Iodine Propulsion Technology, Applications to Low-Cost Lunar Missions, and the iodine Satellite (isat) Project.

Vector-R Forecasted Launch Service Guide

VEGA SATELLITE LAUNCHER

Artemis: A Reusable Excursion Vehicle Concept for Lunar Exploration

Air Platforms Community of Interest Update

Canisterized Satellite Dispenser (CSD) As A Standard For Integrating and Dispensing Hosted Payloads on Large Spacecraft and Launch Vehicles

Space Exploration Via Technology Demonstration and Small Satellite Missions Flown on Reusable Launch Vehicles SSC04-X-8.

Design Reliability Comparison for SpaceX Falcon Vehicles

Transportation Options for SSP

Performance Evaluation of a Side Mounted Shuttle Derived Heavy Lift Launch Vehicle for Lunar Exploration

AFRL Rocket Lab Technical Overview

Transcription:

Upper Stage Evolution Mark Wilkins Atlas Product Line VP United Launch Alliance AIAA_JPC080309 Copyright 2009 United Launch Alliance, LLC. All Rights Reserved.

EELV Sustainment Through 2030 ULA s Evolution Strategy EELV Configurations (3) Upper Stages (2) Avionics Systems (2) GC3 Systems (2) Upper Stage Engines Existing Intermediate Market Common Subsystems Existing Heavy Market Future Heavy & Growth Markets Atlas ULA Consolidation Phase Fleet Optimization Phase 1 Common Upper Stage Phase 2 Booster & GSE Optimization Phase 3 Next Generation System Development Fleet Evolution Delta AIAA_JPC080309 1

Common Upper Stage Enables Robust Industrial Base Avionics Delta IV Upper Stage System Integration Lab Ground/Airborne Software Propulsion Centaur Vehicle Instrumentation Common Airborne & Ground Systems Booster and Payload Interfaces Health Monitoring Ground Computer Systems Launch Sites RL10B-2-1 RL10A-4-3 Space-Based Range Advanced Telemetry Payload Fairing PLF Tri-Sectors Single PLF Recommendation Metallic Tri-Sector 5.1m Composite Next Generation Engine Supplier Viability Through Consolidations & Rate Assured Access Through Reliability, Resiliency & Rate Industrial Base Health Through Sustained P3I Reduced Obsolescence Costs 5.4m Composite Some images courtesy of Pratt & Whitney Rocketdyne AIAA_JPC080309 2

Upper Stage Engine Roadmap 46 klb Prop 61 klb Prop 90 klb Prop RL10A-4-2 Centaur 22 klb RL10B-2 Delta IV 24 klb RL10A-4-3 RL10B-2-1 RL10 Evolution Common Atlas/Delta USG Funded Enhancements Early Fielding with Existing Product Lines Next Gen Engine (Increased Thrust) Requirement Definition MR Isp Cost Some images courtesy of Pratt & Whitney Rocketdyne AIAA_JPC080309 3

EELV Evolution Flexible Mission Architectures Operational Phase 1 Phase 2 Phase 3 20t Class Low Risk Development 40t Class 70t Class Atlas V 100+ t Class 5m Tanks Upper Stage Evolution Dual RD 180s New MLP 30t Class 50t Class 90t Class Delta IV Incl RS-68A 2 or 4 LRB s Solids Existing Launch Pads New Launch Pads Engine Development First Step: Upper Stage Consolidation/Evolution AIAA_JPC080309 4

Mission Needs Drive ULA s Evolution Strategy Lunar Missions Interplanetary C3>0 L1 Telescopes, Cargo, etc. GEO Dual-Satellite Auxiliary Payloads GPS Nav ISS GEO MEO LEO Responsive Launch AIAA_JPC080309 5

Advanced Common Evolved Stage Key Elements Vehicle Equipment Equipment Shelf Monocoque Tank Vapor Cooled Skirt Payload Adapter LO2 Tank LH2 Tank Next Generation Engine Common Bulkhead Combine Best of Atlas & Delta Characteristics AIAA_JPC080309 6

Long Duration Innovation Guided by Flight Experience Reduced LH2 Surface Area LH2 Tank Sized for Substantial Boil-Off MLI & Sun Shield Monocoque Tank Thermal Management Mass Fraction >0.9 Minimal Penetrations Enhanced IB Insulation Internal Sump Supporting Enhanced Mission Requirements AIAA_JPC080309 7

Advanced Common Evolved Stage Extensibility EELVs In-Space Key Elements & Innovations Propellant Depot Lunar Lander Providing Efficient High-Energy Propulsion Core AIAA_JPC080309 8

Ride Share Opportunities Upper Stage Extensibility Image courtesy of Cal-Poly P-Pod Poly PicoSat Orbital Deployer 10 kg ABC Aft Bulkhead Carrier 80 kg CAP+ C-Adapter Platform+ 100 kg Image courtesy of STP Program Office Upper Stage Framework Provides Innovations in Accommodating a Variety of Rideshare & Science Missions Image courtesy of STP Program Office ESPA EELV Secondary P/L Adapter 200 kg/ea IPC Integrated Payload Carrier 500+kg AIAA_JPC080309 9

Summary Atlas V & Delta IV Upper Stages Evolved from Over 100 Years & 1,300 Launches Combined to Achieve the Reliability & Agility Necessary to Serve Today s Broad Launch Needs Active Flight Learning Produces System Knowledge & Reliability for Evolution & Innovation Common System Elements Establish a Framework for Supplier & Industrial Base Health Tank Design Innovations Currently Underway Establish a Framework for Future Missions (Growth & Extensibility) Future Mission Models Benefit from Early Fielding on Current Vehicles & Evolutionary Approaches Strong Systems Engineering Heritage of Disciplined Evolution Provides Capability & Reliability Necessary to Meet Tomorrow s s Space Goals AIAA_JPC080309 10