V100280_Cook_v21

www.dynetics.com

V100280_Cook_v21

October, 2011October, 2011

Dynetics Space Systems OverviewDynetics Space Systems Overview

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Space vehicle development and operations (FASTSAT) End to end missile defense and ASAT modeling and simulation Small, responsive delivery systems

Liquid and solids Components and systems Fabrication Engineering services Testing

EO/IR Radar Laser Hyperspectral Acoustic, magnetic,

seismic Thin film Flight platforms

integration

Ascent and orbital flightmechanics

Propulsion integration Structural analysis Targets and precision guided weapons

Space weather Data analysis from

space observatories

Space Systems Capabilities

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Dynetics Developing Responsive Launch to Support New Markets(US Army SMDC Responsive Space Efforts)

Kestrel Eye

Small Agile TacticalSatellites (SATS)

SMDC – ONE

NanoEye

< 4 kg, 3U Cubesat Form Factor UHF Comm 8 Flight Ready Satellites Data Exfiltration/OTH Comm

10 Kg 1.2-m EO ground resolution Taskable from theater; imagery Downlinked directly to theater

< 25 kg 10-inch telescope EO/IR satellites in LEO Nadir EO resolution of

0.8 m at 300 km

6U Cubesat form factor 3-m EO ground resolution Cassegrain telescope Deployable solar arrays (5U

X 3U)

Multipurpose Nano-Missile System (MNMS)

Extremely simple/low cost missile Augmentable with ATACMS/MLRS

motors 10-kg orbital Nanosat launcher Target Vehicle, Sensor Exerciser Technology Flight Demonstrator

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Fast Affordable Science & Technology Satellite(FASTSAT)

Minisatellite for science, research and technology payloads (< 180 kg)

Affordably enabling a broad range of responsive payloads and missions

Rapid access to space (18 to 24 months) Multiple payload capacity (6) On-Orbit CubeSat deployment (4 x 3U) ESPA class “secondary” launch

compatibility Collaborative development by Dynetics,

NASA Marshall Space Flight Center, DoD Space Test Program, and Von Braun Center for Science and Innovation (VCSI)

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Lunar Lander Testbed: Propulsion Partnership with MSFC

Supporting NASA to demonstrate and mature technologies for future robotic space exploration missions

Designed, built, tested, delivered cold-gas propulsion system for a testbed; ATP to delivery in 14 weeks

Recently delivered new flight weight H2O2 flight system in 10 months 12 ACS thrusters, 3 descent thrusters,

and 1 Earth Gravity Canceling thruster

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Rideshare Finances Landing Commercially on the Moon

ESPA Tug

Rocket City Lander

The Rocket City Rover