main commercial crew program overview collura
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Commercial Crew Program
National Aeronautics and Space Administration
Commercial Crew Program OverviewMasters Forum 20
Maria ColluraApril 22, 2011
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CCP Objective
2
CCP is leading NASAs efforts to develop an American-made
commercial capability for crew transportation and rescue services
to the ISS following this year's retirement of the space shuttle fleet
Kennedy Space Center will host theprogram office dedicated to enablingcommercial human spaceflightcapabilities.
Program Manager (PM) will
reside at KSC Deputy Program Manager
located at JSC
Program Mission Manage the investment in the
development of commercial end-to-
end space transportation systems Manage the CTS (Crew TransportationSystem) certification process
Lead the technical and programmaticpartner integration and approvalfunctions
http://moonpans.com/prints/Apollo_9_CSM.jpg -
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CCP Organization
3
Partner Team
(Sierra Nevada)
Partner Team
(Space X)
Partner Team
(Blue Origin)
Partner Team
(Boeing)
SystemsLaunch Vehicle
Spacecraft
Launch & Recovery Systems
Mission Planning & Integration
Systems Engineering
& Requirements
Program Control &
IntegrationPartner Integration
FAACommercial Crew Program
Technical
Authority
ISS Program
LSP Program
C3PO Program
Human
Exploration &
Operations
Directorate
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CCT-1100 Series Documents
4
ESMD-CCTSCR-12.10
CCT-DRM-1110
SSP 50808CCT-REQ-1130
CCT-STD-1140 CCT-STD-1150
CCT-PLN-1100
Crew Transportation Design Standard Guidelines - provides
expectations, and criteria used in evaluation of technical
standards
Crew Transportation Operations Standard Guidelines - provides
expectations for minimum criteria and practices for operations
High Level Program Summary of roles, responsibilities, and interfaces
between CCP and partners in the development of CTS, and How NASA and
the CP will work together to achieve a Certified Human Flight Vehicle
ISS Visiting Vehicle Requirements -must comply with to
interface with the International Space Station
Crew Transportation and Services Requirements -must meet to
transport NASA Crew to the ISS
Crew Transportation System DRMs potential reference missions for current
and evolvable systems architecture designs
Agency and HQ Level Requirements levied on the Program intended to certify a CTS to carry a NASA crewmember to LEO
CCT-PLN-1120
Crew Transportation Technical Management Processes summary of technical
management processes that support certification and expectations for evidence
of compliance
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Insight/Oversight Model Level of Involvement
NASA will perform insight/oversight on the Commercial Partnersdesign, development, and certification process to evaluate the end-to-
end crew transportation systemHuman
Spaceflight
Launch ServicesProgram
Intense In/OversightLow In/Oversight
Scientific & Commercial Spacecraft--Contracted
COTS &CRS
CommercialCrew
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Commercial Crew Structure and Timelines
6
2012
FebruaryAwardsCCDev
2011
CCDev Round 2
CCDev Round 3
2010Title Purpose
AprilAll Agreements
Complete
Octob
er
Announcementfor Proposals
April
Awards
May
AgreementsComplete
Develop and demonstratetechnologies that enablecommercial humanspaceflight capabilities.
Mature the Design andDevelopment ofelements of the system,
such as launch vehiclesand spacecraft.
Design of integratedcommercial crewsystems.
Today
CCPMature Development, Testand Certification of end-to-end systems.
Prepared for services toISS by end of 2016.
2013-2016
Pre-DecisionalNASA Internal Use Only
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Commercial Crew Development (CCDev)
7
The NASA Recovery Act stimulus funding,included $50M to stimulate efforts within theprivate sector to develop and demonstratetechnologies that enable commercial humanspaceflight capabilities
On February 1, 2010 five partners were
announced and received funding: Blue Origin Boeing Paragon Sierra Nevada Corporation United Launch Alliance (ULA)
All Agreements were concluded by December2010, with the exception of ULA and Boeing whoreceived no-cost extensions to April 2011
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Commercial Crew Development Round 2CCDev2
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CCDev 2 Summary
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Participant Name Work Summary NASA Funding
Blue OriginSpace Vehicle design to SRR, pusher escape ground and flight
testing, and engine pump and thrust chamber testing$22,005,000
BoeingCST-100 design maturation to PDR and launch vehicle
integration$92,300,000
Sierra Nevada CorporationDream Chaser crew transportation system design maturation
to PDR and component testing$80,000,000
SpaceXSide-mount LAS engine design maturation and partner-funded
crew accommodation prototype$75,000,000
Total Funding $269,305,000
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Blue Origin
Subs/Suppliers:
NASA Ames Research Center Aerojet
NASA Stennis Space Center Lockheed Martin Missiles & Fire Control HSWTULA U.S. Air Force Holloman High Speed Test Track
Description & Features:
Launch vehicles Atlas V
Then on their own Reusable Booster System (RBS)
Biconic shape capsule spacecraft Composite structure
Landing system trade study Pusher Escape System Testing Fully Reusable Booster System (RBS)
Post separation, RBS will either ballistic trajectorydownrange or restart engines to return to launch site
Comments: Direct docking to ISS Vehicle Mass: 22,000 lbm
Time
SV + Atlas VGoddard CC + PM
Low Altitude
Suborbital
Orbital
SV + RBS
Design ReviewsSRR PDR
May 2012 ---
Capacity Summary kg/Flt Max Crew--- 7
Flare
Bi-directionalFins
Deep-throttling
Engines
Total NASA funding $22M
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Boeing
Description & Features:
Launch vehicles Atlas V 412, Delta IV Compatible with Liberty and F9
CST-100 is a reusable capsule spacecraft Land landing on airbags Integrated bi-propellant SM propulsion
system
Comments:
Direct docking to ISS 48 hours of autonomous flight operations Vehicle Mass: 30,430 lbs
123456-006
Ascent Cover
LAS RollThrusters(8)
Launch AbortEngine (LAE) MMOD/Thermal Shield
OrbitalManeuvering,Attitude Control(OMAC)
SM RCSThrusters(28)
Forward Heatshield
Side Hatch
CM-SMUmbilical
Thruster Doghouse (4)Radiators (4)
Forward Window
Side Window
CM RCSThrusters (12)
Design ReviewsDelta SDR PDR
May 2011 April 2012
Capacity Summarykg/Flt Max Crew
1,164 7
Subs/Suppliers:Airborne Systems United Space AllianceBA United Launch AllianceILC Dover PWRSpincraft
Software Development and Integration
Pre-launch processing Cargo loading Final test and checkout Fueling Ordnance installation Encapsulation
Assembly, refurbishment and test Spacecraft element production Element test and checkout
Recovery Initial safing
Crew egress
Cargo removal Load on transporter Transport to manufacturing
for potential reuse
MECO LV staging Spacecraft separation LV disposal
Orbitalinsertion
SMseparation
SM disposal
De-orbit burn
Rendezvous/proximity operations Docking Mated operations Crew Cargo transfer
Crew ingress De-orbit preps Un-docking Separation
Pad operations Spacecraft arrival
at launch pad Hoist and mate to
launch vehicle Late cargo loading
Crew ingress Countdown Launch
Orbitaloperations
Launch
LandingMission
control
Spacecraft operations control Mission planning Ground processing ops control Crew training Cargo manifesting Integrated testing Launch operations Orbital command and control Landing and recovery control
Flight, Ground, Mission Ops SW Dev Avionics HW/SW and ISS Integration testing Mission / Vehicle Common Data System 193879-011.pptx
Total NASA funding $92M
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Sierra Nevada Corporation
Subs/Suppliers:United Launch Alliance United Space Alliance
AEROJET Draper Laboratory
Adam Works SAS
Boeing Virgin Galactic
MDA University of Colorado
NASA LaRC
Description & Features: Launch vehicles
Atlas V-402 Investigating other options (ATK Booster)
Dream Chaser is a Reusable Piloted Lifting Body,Derived from NASA HL-20
Onboard hybrid propulsion & high lift providerunway landings for nominal missions and ascentaborts
Comments:
Direct docking to ISS Vehicle Mass: 27,100 lbm Multiple & Flexible Abort Options (no black zones)
Design ReviewsSRR PDR
May 2011 May 2012
Capacity SummaryCargo (kg/Flt) w/Crew Max Crew
1,500 2 7
Total NASA funding $80M
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SpaceX
Description & Features: Dragon Capsule Spacecraft
Cargo version to evolve into crew version
Many systems identical in both Integrated LAS development and crew
accommodations are the focus for CCDev2
Water landing (helicopter recovery) forearly missions and land landing for latermissions
Comments: Falcon 9 Launch Vehicle
Two-stage LOX and kerosene Falcon 9/Dragon launches
Successful COTS launch 12/8/10 11 more scheduled before crew launchFlight-proven
and common
to cargo andcrew D ragon
Propulsive,
precise
system partof long-term
capability
Offerssignificant
advantagesover tower
systemsWINDOWS
Flight-proven
and commonto cargo andcrew Dragon
DRACO THRUSTERS
GROUND LANDING
INTEGRATED LA S
SpaceX system
has large
factor of safetyfor ISS reentry
PICA-X
DRAGON AT A GLANCE
Design ReviewsLAS PDR Concept Baseline Review
Sept 2011 May 2012
Capacity Summary
kg/Flt Max Crew
--- 7
Subs/Suppliers:ARES Corporation Paragon SDCOdyssey Space Research ILC DoverATA Engineering OceaneeringWyle Laboratories Orbital OutfittersInformation Systems Laboratories Inc.
Total NASA funding $75M
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A successful Commercial Crew Program will:
Transform human spaceflight for future
generations
Result in safe, reliable, cost effective crew
transportation to LEO and in support of ISS
Free NASAs limited resources for beyond-LEO
capabilities Reduce reliance on foreign systems
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