Boeing Commercial Crew Transportation System Keith Reiley Boeing

Boeing Commercial Crew Transportation System Keith Reiley Boeing Commercial Crew DPM FISO Telecon February 6, 2013

Content • CSTS Overview • Operations Concept • Vehicle Features • CCDev 2 and

Boeing Brings History of Human Space Flight & Commercial Airplanes Together Copyright © 2011

Commercial Crew Transportation System (CCTS) • Complete transportation system – Commercial Crew Vehicle – Launch Vehicle – Ground Operations – Mission Operations – Recovery • Design objectives dictate uncomplicated systems and proven components – Safe and reliable – Low development risk – Low recurring cost • Compatible with a variety of launch vehicles – Have down selected to Atlas V for initial flight tests and verification Boeing CST-100 Partners & Subs Bigelow Aerospace PWR General Dynamics Airborne Systems Spincraft • Operational in 2016 Copyright © 2012 Boeing. All rights reserved. 4

Concept of Operations Copyright © 2012 Boeing. All rights reserved. 5

Spacecraft Segment (CST-100) Ascent Cover Forward Window Side Hatch Crew Module Umbilical CM SM

Launch Abort System • Provides abort capability from the launch pad through Earth-orbit insertion, protecting against: – Complete or partial loss of ascent Bantam Engine thrust/propulsion – Loss of attitude or flight path control –Time-critical system failures Launch Abort Engine Test Firing No “Black Zones” OMAC RCS Engine Test Firing Copyright © 2012 Boeing. All rights reserved. 7

CST-100 Key Design Features Crew of Seven or Combination of Crew and Cargo Reusable Crew Module (CM) Expendable Service Module (SM) Liquid Propellant Launch Abort System Landing on Airbags Copyright © 2012 Boeing. All rights reserved. 8

CM Internal Layout Landing Attenuation Seat Struts Avionics and Software Integration lab ECLSS Crew/Cargo

CST-100 Design Evolution IDR-1 IDR-2 IDR-3 ISR SDR PDR IDR-4 Copyright © 2012 Boeing.

Landing Opportunities Nominal returns to WSMR Edwards AFB available for additional landing opportunities Emergency

CST-100 CCDev Design Landing Drop Tests Copyright © 2012 Boeing. All rights reserved. 12

CM/SM Assembly in KSC OPF-3 Fueling Operations Before Flight Base Heat Shield Installation Copyright

CCi. Cap Base Period Major Milestones 2013 -2014 Copyright © 2012 Boeing. All rights

CCTS Design Maturation Under CCi. Cap Aug. 2012 through Jan. 2013 § Integrated System Review – Established and demonstrated CCTS Vehicle and operations that meets system requirements § Production Design Review – Established the baseline plan, equipment and infrastructure for performing the manufacture, assembly and acceptance testing of the CST-100 – Leveraged successful and extensive Boeing Commercial production practices § Phase 1 Safety Review Board – Conducted a comprehensive safety review to access conformance with NASA’s Crew Transportation System certification process – Focused on hazard reports, cause descriptions and controls § CST-100 Interior Layout Evaluation – Completed three-day evaluation with NASA astronauts on reach and visibility of controls/displays – Received feedback on the design of the crew seats, interior lighting, and optimum layout for Crew Resource Management § Software Engineering Release 2. 0 – Initial release of flight software § Landing & Recovery/Ground Comm. Design Review – Preliminary design of ground and communications architecture Copyright © 2012 Boeing. All rights reserved. 15

CCTS Design Maturation Under CCi. Cap 2013 Milestones Boeing’s CCTS 2013 Plan: – Continue system design maturation – multiple demonstrations – CST-100, Atlas V integration and Launch Pad Modifications – Mission Control demonstrations – Continued re-development of the ULA Dual Engine Centaur – Launch Vehicle Adapter PDR & CDR – Continued development of KSC OPF-3 Copyright © 2012 Boeing. All rights reserved. 16

CCi. Cap Risk Reduction Demonstrations • • Phase II Wind Tunnel Tests OMAC Engine Development Test LV EDS Test DEC Liquid Oxygen Duct Development Test • Avionics and Software Multi-string Demonstration Test • Pilot-in-the-Loop Demonstrations Copyright © 2012 Boeing. All rights reserved. 17

Full Crew Transportation Capability by 2016 • CST-100 takes advantage of heritage hardware to reduce schedule risk – Orbital Express demonstrated AR&D – Apollo heritage parachute system – Abort system using existing components – Avcoat from Apollo – Delta-based spin formed structures – Airbag landing system from Boeing CEV/Orion 2010 SDR 2011 2012 PDR CCDev-2 2014 2015 2016 CDR Structural Test Article Pad Abort Test CCi. Cap Orbital Flight Test (uncrewed) Two-Crew Flight Test Air Bag System Integrated AR&D System Copyright © 2012 Boeing. All rights reserved. 2013 Apollo/Orion Heritage Avcoat SM Abort Engine Heritage Parachute System Weldless Structure Simple, Passive Life Support Systems 18

Boeing Commercial Crew Summary • Significant Progress to date under CCDev, CCDev-2, and CCi. Cap – All milestones completed to plan – Critical Design Review in Apr, 2014 • Low Risk, Low Cost Development – Simple systems – Existing technologies – Proven launch vehicles – NASA’s acquisition approach caps costs through firm milestone values – Demonstrated commercial development approach with NASA involvement • Low Operational Costs – Leveraging Boeing’s commercial aircraft experience – Multiple mission capsule Reliable, Safe Transportation Soon Affordable Access to LEO Enables Exploration Beyond LEO Copyright © 2012 Boeing. All rights reserved. 19