Commercial Crew Cargo Program Status Conference on Quality

  • Slides: 22
Download presentation
Commercial Crew & Cargo Program Status Conference on Quality in the Space and Defense

Commercial Crew & Cargo Program Status Conference on Quality in the Space and Defense Industries Cape Canaveral, Florida March 15, 2011 Mark Erminger Chief Safety and Mission Assurance Officer Commercial Crew & Cargo Program Exploration Systems Mission Directorate Johnson Space Center

Program Objectives l The Commercial Crew & Cargo Program was established in November 2005

Program Objectives l The Commercial Crew & Cargo Program was established in November 2005 to accomplish the following objectives: u Implement U. S. Space Exploration policy with investments to stimulate the commercial space industry u Facilitate U. S. private industry demonstration of cargo and crew space transportation capabilities with the goal of achieving safe, reliable, cost effective access to low-Earth orbit u Create a market environment where commercial space transportation services are available to Government and private sector customers Extending human presence in space by enabling an expanding and robust U. S. commercial space transportation industry 2

Safety is Built Into the Design and Development Process l NASA Reviews S&MA Products

Safety is Built Into the Design and Development Process l NASA Reviews S&MA Products During Partner Design Reviews u Safety and Mission Assurance Plan u Quality Plan u Hazard Analysis u Safety Assessments u Risk Assessments u Probabilistic Risk Assessment u Software Assurance l COTS partners are required to obtain an Federal Aviation Administration license for all of the demonstration missions l COTS partners are required to meet all Space Station visiting vehicle requirements and be approved by the Space Station Safety Review Panel (SRP) before being allowed to rendezvous and berth with the ISS 3

Space. X COTS System Description and Features: l Falcon 9 Medium Class Launch Vehicle

Space. X COTS System Description and Features: l Falcon 9 Medium Class Launch Vehicle l Dragon Crew/Cargo Spacecraft l Recoverable launch vehicle and spacecraft l Cape Canaveral LC-40 Launch Site l ISS Flight Demonstration l NASA Investment: Dragon Cargo Capsule Falcon 9 Rocket Dragon Crew. Capsule u Cargo Demonstration – up to $278 M u Crew Demonstration Option– up to $308 M (not funded) Space. X Launch Site at Cape SLC 40 4

Space. X COTS Demo Mission 1 5

Space. X COTS Demo Mission 1 5

Orbital COTS System Description & Features: l Taurus II Launch Vehicle – derivative of

Orbital COTS System Description & Features: l Taurus II Launch Vehicle – derivative of Taurus I with Aerojet AJ-26 engines (2) & Castor 30 2 nd stage l Cygnus Service Module used for all missions – derived from STAR™ & Dawn spacecrafts l Pressurized Cargo Module (PCM): Heritage - ISS MPLM Taurus II Rocket l Wallops Flight Facility Launch Site l ISS Flight Demonstration Pressurized Cargo Module & Service Module l NASA Investment: u Cargo Demonstration – up to $170 M Taurus II MARS/Wallops Launch Site 6

Orbital COTS Mission Visualization 7

Orbital COTS Mission Visualization 7

WFF Pad 0 A Construction Progresses 8

WFF Pad 0 A Construction Progresses 8

Taurus II First Stage Test Article Arrives at WFF 9

Taurus II First Stage Test Article Arrives at WFF 9

PCM Integration & Testing PCM 1 PCM 2 PCM 0 10

PCM Integration & Testing PCM 1 PCM 2 PCM 0 10

AJ-26 Engine at Stennis for Testing 11

AJ-26 Engine at Stennis for Testing 11

ULA CCDev 1 Project • Developed a modular Emergency Detection System (EDS) which can

ULA CCDev 1 Project • Developed a modular Emergency Detection System (EDS) which can be used with Atlas V, Delta IV, and other LVs • CCDev 1 tasks: EDS definition Identified LV failure modes and how measured Algorithm development, software coding, validation • Crew interface design • Prototype EDS tested and demonstrated • Real-time monitoring demonstration • • NASA invested $6. 7 M Partners & Subs Pratt & Whitney SAS 12

ULA Emergency Detection System 13

ULA Emergency Detection System 13

Blue Origin CCDev Project • System concept is bi-conic space vehicle launched on Atlas

Blue Origin CCDev Project • System concept is bi-conic space vehicle launched on Atlas V 402 • Matured Pusher Escape System • • Conducted TVC ground testing Matured Composite Pressure Vessel • Manufactured structural test article of a suborbital capsule as a subscale demonstrator for the orbital Space Vehicle • • • Over-pressurized the test article Conducted pressure vessel drop test NASA investment $3. 7 M 14

Blue Origin Composite Crew Pressure Vessel and Thrust Vector Control Testing

Blue Origin Composite Crew Pressure Vessel and Thrust Vector Control Testing

Paragon CCDev Project • Developed Air Revitalization System (ARS) for commercial crew • Matured

Paragon CCDev Project • Developed Air Revitalization System (ARS) for commercial crew • Matured its ARS concept under CCDev • Requirements development with 4 potential • • vehicle providers Designed through PDR level Manufactured and tested an engineering development unit • NASA investment $1. 44 M Partners & Subs Micropore TDA Research Perma Pure Barber Nichols Vista Photonics 16

Paragon CCDev 1 Air Revitalization System Engineering Development Unit 17

Paragon CCDev 1 Air Revitalization System Engineering Development Unit 17

Boeing CCDev 1 Project • Commercial Crew Transportation System concept: ¨ ¨ ¨ Flexible

Boeing CCDev 1 Project • Commercial Crew Transportation System concept: ¨ ¨ ¨ Flexible crewed vehicle concept with maximum of seven crew Light-weight design compatible with Atlas, Delta, and Falcon 9 Integrated operations & crew training center • Matured system architecture and design through SDR and demonstrated key technologies and capabilities via 9 tasks ¨ ¨ ¨ ¨ ¨ Partners & Subs SDR Abort System Hardware Demonstration Base Heat Shield Fabrication Demonstration Avionics Systems Integration Facility Demonstration CM Pressure Vessel Fabrication Demonstration Landing System Demonstration Life Support Demonstration AR&D Integrated GNC Demonstration Crew Module Mockup Demonstration • NASA investment $18 M Bigelow Aerospace Aerojet Airborne Systems ATK Spincraft 18

CST-100 CM Pressurized Structure Fabrication & Test 19

CST-100 CM Pressurized Structure Fabrication & Test 19

Sierra Nevada CCDev 1 Project • • Partners & Subs Boeing Draper Lab ULA

Sierra Nevada CCDev 1 Project • • Partners & Subs Boeing Draper Lab ULA Aerojet Adam. Works MDA University of Colorado • • • Commercial STS based on NASA HL-20 launched on Atlas V Requirements defined for Dream Chaser systems design & major subsystems Built & Tested Spacecraft Primary Structure Integrated Loads Defined & CFD studied Main Propulsion Motor Built & Tested RCS Thruster Prototype Built & Tested Developed Atmospheric and Orbital GN&C architecture Flight Algorithms & Software Assurance Plan TPS Trades completed Atlas V Integration analyses Scale Dynamic Model Flight Tested NASA investment $20 M 20

SNC Dream Chaser Structural & Propulsion System Testing 21

SNC Dream Chaser Structural & Propulsion System Testing 21

22

22