Shared Ride Opportunities OnOn Orbital Launch Vehicles · • Orbital MACH avionics module • Cold-gas 3-axis Attitude Control System Available Through NASA STAGE 1 • Liquid Oxygen/RP-1

Shared Ride OpportunitiesShared Ride OpportunitiesOnOn

Orbital Launch VehiclesOrbital Launch Vehicles

Warren Frick11 June 2014

1

© 2014 Orbital Sciences Corporation. All Rights Reserved.

8-LSG GNLR-0125

Orbital Overview

Leading Developer and Manufacturer of Small- and Medium-Class Space Systems 30-Year Record of Reliable, Rapid and Affordable Development and Production Serving Customers in Commercial National Security and Civil Government Markets Serving Customers in Commercial, National Security and Civil Government Markets

Over 1,050 Satellites and Launch Vehicles Built or Under Contract for Customers 215 Satellites and Space Systems 215 Satellites and Space Systems 179 Space and Strategic Launch Vehicles 661 Target Vehicles and Sounding Rockets

3,500 Employees and 1.6 Million Square Feet of State-of-the-Art Facilities

Revenues of About $1.5 Billion Expected in 2014p

Contract Backlog Totals $4.8 Billion for Delivery Through 2018

2Orbital SPRSA Briefing 2014

Conservative Balance Sheet With Strong Liquidity


8-LSG GNLR-0125

Well-Balanced Business Segments

Satellites and Space Systems Launch Vehicles Advanced Space Programs

35%

35% 30%

2014 Revenues ~$1.5 Billion 3Orbital SPRSA Briefing 2014


8-LSG GNLR-0125

Launch Systems Experience

Space Launch Vehicles Strategic Launch Vehicles Target Vehicles Small Payloads (Up to 2 Tons) Medium Payloads (3 to 7 Tons) Special Purpose Vehicles Mission Record

Interceptor Vehicles Global Strike Vehicles ICBM/IRBM-Class Targets Mission Record

Short-Range Targets Medium/Intermediate Targets Special Purpose Vehicles Mission Record

76 Launches Since 1982 93% Mission SuccessProduction Backlog 1 Unit Delivered

24 Launches Since 1982 100% Mission SuccessProduction Backlog 42 Units Delivered

175 Launches Since 1982 95% Mission SuccessProduction Backlog 28 Units Delivered

11 Units in Backlog 24 Units in Backlog 46 Units in Backlog 112 Major Launches With Over 97% Success in Last 10 Years



8-LSG GNLR-0125

Orbital’s Space Programs

Pegasus XL

Minotaur I

Minotaur IV

Antares

Minotaur V

Minotaur VI

5

Minotaur-C 12 Different Space and Strategic Launch Vehicles DevelopedOver 75 Space Missions Launched Over the Last 20 Years

Orbital SPRSA Briefing 2014


8-LSG GNLR-0125

Orbital’s Space Launch Vehicle Capabilities

Antares

(West Coast Launch)

Minotaur VI

Minotaur IV

LEO (200km x 38°)

HI/VAFP (600km x 90°)

HI/WFF (600km x 90°)

Minotaur I

Minotaur ‐C

Pegasus XL

Vehicles Ideally Suited To MeetSmall to Medium Launch Requirements

0 1000 2000 3000 4000 5000 6000 7000

kg6Orbital SPRSA Briefing 2014


8-LSG GNLR-0125

Pegasus XL - Small Space Launch to Any Inclination

Air-Launched, Winged, 3-Stage Solid Motor

Advanced Composite Materials

Space Launch Vehicle

Operations Based at Vandenberg AFB, System Mobility Allows Wide Flexibility in Stage 2

Stage 3Orion 38 Motor

System Mobility Allows Wide Flexibility in Launch Location and Mission Orbits

42 Missions With 28 Consecutive L-1011 Launch

Stage 1Orion 50 SXL Motor

Orion 50XL Motor

Successes Since 1997Only Small Space Launch Vehicle

Certified by NASA for yCategory 3 Payloads

Available Through NLS II andgCommercial Contracts

Launch Sites/Orbits7Orbital SPRSA Briefing 2014


8-LSG GNLR-0125

MinotaurMulti‐Stage Solid Propulsion Launch Vehicles with Common Avionics, Structures and Combinations of:

Refurbished ICBMMotors

Minotaur I4 Stage

(2 GFE, 2 New)

Minotaur V5 Stage

(3 GFE, 2 New)

Minotaur IV4 Stage

(3 GFE, 1 New)

Minotaur VI5 Stage

(4 GFE, 1 New)

4 Space Launch Configurations Available, Providing Ability to Tailor Vehicle

Refurbished ICBM MotorsNew Build Upper Stage Motors

100% Launch Reliability on 25 Missions Over the Last 14 Years

Providing Ability to Tailor Vehicle Performance to Mission Needs

Over the Last 14 Years

Compatible with All FourMajor US Launch Sites

Ideal Delivery System for Disaggregated

New USAF OSP‐3 Contract Award Provides Availability for DoD Missions Minotaur I at

Vandenberg AFB

Ideal Delivery System for DisaggregatedArchitecture Systems

Minotaur IV at Kodiak Launch Complex

8Minotaur V at Wallops



8-LSG GNLR-0125

Minotaur-CAffordable Commercial Small Launch Capability

Commercial Variant of Minotaur

Compatible With US Stage 3Compatible With US Spaceports at Wallops, Kodiak,

Vandenberg, and Florida

Utili E i ti Fli ht P

Stage 2Orion 50 XL Motor

Stage 3Orion 38 Motor

Utilizes Existing, Flight Proven Hardware and Software From

Minotaur, Taurus, and Pegasus to Reduce Risk

Stage 1Orion 50 XLT Motor

to Reduce Risk

First Mission on Contract for SkyBox, Deploying 6 Satellitesy p y g

Available Through NLS-II and Commercial Contracts

Stage 0CASTOR 120 Motor

9Launch Sites/OrbitsOrbital SPRSA Briefing 2014


8-LSG GNLR-0125

Antares

PAYLOAD FAIRING• 3.9 meter diameter by 9.9 meter envelope• Composite Construction

Designed to Replace Delta II

Currently Under Contract to Support NASA

International Space Station STAGE 2• ATK CASTOR® 30B/30XL Solid Motor with

Active Thrust VectoringO bit l MACH i i d l

Composite Construction• Non-contaminating Separation Systems

(ISS) Re-supply Missions (10 Missions Thru 2016)

STAGE 1

• Orbital MACH avionics module• Cold-gas 3-axis Attitude Control System

Available Through NASA STAGE 1• Liquid Oxygen/RP-1 fueled• Two AJ26 engines with independent

thrust vectoring – 740,000lbf Thrust (SL)• 3.9 meter booster derived from

heritage Zenit design

Available Through NASANLS-II Contract

Available Through USAF

VEHICLE PARAMETERS• Gross Liftoff Mass: 290,000 – 310,000 kg• Vehicle Length: 40 m• Vehicle Diameter: 3.9 m

heritage Zenit designOSP-3 Contract

Available Commercially Vehicle Diameter: 3.9 m• Mass to ISS Orbit: 5000 kg Baseline

6265 kg Enhanced

y



8-LSG GNLR-0125

Orbital Space Launch Contracts & Manifest

Year Vehicle Payload / Program

2013 Antares Pegasus XLAntares

Test LaunchIRIS

COTS Demo

ProgramAvailability

NLS‐II OSP‐3 Commercial

AntaresMinotaur VMinotaur I

COTS DemoLADEEORS‐3

2014 AntaresAntaresAntares

CRS ORB‐1CRS‐ORB‐2CRS‐ORB‐3

Vehicle

Pegasus X X

Minotaur‐C X X Antares CRS‐ORB‐3

2015 AntaresAntares

Minotaur‐C

CRS‐ORB‐4CRS‐ORB‐5Skybox 1

2016 Antares CRS‐ORB‐6

(Taurus XL)

Minotaur X

Antares X X X

AntaresAntares

Pegasus XLPegasus XLMinotaur‐CMi

CRS‐ORB‐7CRS‐ORB‐8CYGNSSAvailableAvailableA il blMinotaur

AntaresAvailableAvailable

FlownContracted

11

ContractedAddressable



8-LSG GNLR-0125

Multiple Payload Hosting Options

Dual Payload Attach Fittings (DPAF) Hosts Several Larger Satellites, Each With Dedicated, Axial Load Paths and Separation

Systems

Multiple Payload Attach Fitting (MPAF) Hosts Multiple Smaller Payloads of Different Classes C bi With O ti O bit Adj t t S t Combines With Options Orbit Adjustment System

CubeSat Delivery Systems PPOD/ISIPoD/CubeStack/EtcO S C S

Hosts Multiple Payload in Defined CubeSat Class

Stacked Satellites L d B i S lli Load-Bearing Satellites

MicroStar (ORBCOMM, COSMIC), and GEOStar

Dispenser Based Dispenser Based



8-LSG GNLR-0125

92” Fairing DPAF (Minotaur IV, VI, -C)

Dual Payload Attach Fitting (DPAF) Qualified and Flown Successfully on Taurus

92” Fairing

Eliminates Challenge of Lower Spacecraft Carrying Loads of Forward Spacecraft

Fli h D l O i i h Flight-proven Deployment Operations with Frangible Joint Separation System to Maintain Cleanliness of Lower S/C

Each S/C can have their own Custom SoftrideSystem to De-couple Loads as Well as Reduce Loads of Concern

P l d S ti S t

DPAF Separation System

Payload Separation System

Additional Spacecraft Within thep y Within the DPAF Cylinder



8-LSG GNLR-0125

50, 61 & 63” Fairing DPAF (Minotaur I,-C, Pegasus)

50” Fairing61 & 63” Fairing PegasusTaurus g38” Wide DPAF

g50” Wide DPAF

PegasusSAC-B / (HETE)

TaurusOrbView-4 /(QuikTOMS)



8-LSG GNLR-0125

92” Fairing MPAF (Minotaur IV, VI, -C)



8-LSG GNLR-0125

Antares Secondary Payload Options

8‐LSG_LaunchSvcs_No License‐0047

Attach to Existing Payload Attach Structure Secondary Separating or Non-separating

Payload or Small-Sat Dispenser Attached U S f A L h V hi lto Upper Stage of Antares Launch Vehicle

PPOD Interface Quoted as Non-Standard Service for NLS and OSP-3

Opportunity Exists for Secondary Payloads Up to ~300 kg

Hosted Payload on Cygnus ISS Resupply Vehicle

Alternative, Third-Party Solutions Under Review for CRS and Non-CRS Missions A-Deck Light Weightg g Andrew’s Aerospace “Sherpa” System EXPRESS System ESPA Class EAGLES Program EAGLES Program



8-LSG GNLR-0125

Orbital’s Multiple PayloadSpace Launch Experience Summary

Orbital Has Averaged >2 Spacecraft/Mission Across All Space Launch Missions 42 Pegasus Missions, 85 Spacecraft: >2/Mission 9 Taurus Missions, 17 Spacecraft: ~1.9/Mission 11 Minotaur I Missions, 53 Spacecraft: ~4.8/Mission

61 Spacecraft, ~5.5/Mission if Tertiary Payload Separations are Counted 4 Minotaur IV and V Missions, 12 Spacecraft 3/Mission

13 Spacecraft Tertiary Payload Separations are Counted 3 Antares Missions , 9 Spacecraft, 3/Mission

Pegasus Minotaur ITaurus Minotaur IV

BATSAT/

JAWSAT/ASUSat/Falconsat‐1/SNOE

GFO/ STPSat‐2/ /

Falconsat‐1/OCS/ OPAL

STPSat‐3/2‐ LoadpathCubeStack

TERRIERS/MUBLCOM COSMIC

ORBCOMM FASTSAT/ FASTRAC/ FalconSat‐5/ RAX/ O/OREOS

CubeStackStructures (16, 3u CubeSatDispensers)Orbital SPRSA Briefing 2014


8-LSG GNLR-0125

Summary

Orbital has Always Supported the Secondary and Tertiary Ride Share Community Our First Pegasus, Taurus, Minotaur I, and Antares Missions Successfully Hosted Multiple

Spacecraft We Look Forward to Continued Support of This Community We Look Forward to Continued Support of This Community

For Additional Information, Please Contact Mark Pieczynski, VP, Space Launch Business Development

(714)677 2444 (714)677-2444 [email protected]

General Launch Vehicle Contacts John Steinmeyer, Senior Program Managery , g g

◦ 714-677-2440◦ [email protected]

Warren Frick, Advanced Projects◦ 703-948-8192◦ [email protected]

Minotaur Specific Contacts Kevin Wilder, Minotaur Program Director

◦ 480 814 6200◦ 480-814-6200◦ [email protected]



8-LSG GNLR-0125

Shared Ride Opportunities OnOn Orbital Launch Vehicles · • Orbital MACH avionics module • Cold-gas 3-axis Attitude Control System Available Through NASA STAGE 1 • Liquid Oxygen/RP-1

Documents