1

SpaceX proprietary

data constitutin

g “Confidenti

al Informatio

n” under applicable

agreements. SpaceX proprietary data constituting “Confidential Information” under applicable agreements.

Tim HughesVice President & Chief Counsel

Falcon 1Falcon 1 Falcon 9Falcon 9 DragonDragon

Space Exploration Technologies Corporation 2Oct. 2, 2008

Falcon 1 Overview

2-stage small launch vehicle Vehicle dia. 5.5’; Fairing dia. 5’; Length 68’ 1st Stage LOX/RP1 Merlin M1 engine, ~78k lbf 2nd Stage LOX/RP1 Kestrel engine, ~7k lbf

vac. Firm fixed price:

$8.1 M all inclusive commercial service (Jan. 2008) Launch from Kwajalein (Reagan Test Site) 1st Stage Parachute/Water Recovery Enhanced Falcon 1 (F1e) block upgrade

planned Available early 2010

Payload capability LEO F1: >1030 lbm (470 kg) F1e: >1580 lbm (720 kg)

Oct. 2, 2008 Space Exploration Technologies Corporation

All structures, engines, most avionics and all ground systems designed (and mostly built) by SpaceX

All structures, engines, most avionics and all ground systems designed (and mostly built) by SpaceX

33

Falcon 1Falcon 1

DockDock

Integration Hanger& Clean-room

Integration Hanger& Clean-room

OfficesOffices

SharksSharksSpace Exploration Technologies CorporationSpace Exploration Technologies Corporation 44Oct. 2, 2008Oct. 2, 2008

Space Exploration Technologies Corporation 5

SLC-40, Cape CanaveralSLC-40, Cape CanaveralCentral TexasCentral TexasHawthorne HeadquartersHawthorne Headquarters

KwajaleinKwajalein

Singular goal of providing high reliability, low cost space transportation

Transition to human transportation once technology is proven

Over 570 employees — grow minimum 50% per year

550,000 sq ft of offices, manufacturing and production in Hawthorne, CA

300 acre state-of-the-art propulsion and structural test facility in central Texas

Launch complexes in Kwajalein and Cape Canaveral

Oct. 2, 2008

2-stage EELV-class launch vehicle Vehicle dia. 12’; Fairing dia. 17’ (5.2 m); Length 180’ 1st Stage LOX/RP1

9 x Merlin M9 engines 2nd Stage LOX/RP1

1 x Merlin M9-vac engine Payload capability (Block 1):

10 MT LEO (KSC 28.5°; 200 km; circular) 3.5 MT GTO 2.1 MT TLI 1.0~1.4 MT Mars (depending on launch date)

Launch from the Cape (LC-40) Vehicle at Cape: Dec. 2008 $36.75M all inclusive commercial cost (Jan. 2008 $) Block upgrade planned in 2010 timeframe F9-Heavy also planned

3-stick configuration 29 MT LEO

All structures, engines, most avionics and all ground systems designed (and mostly built)

by SpaceX

All structures, engines, most avionics and all ground systems designed (and mostly built)

by SpaceX

NASA human-rating Factor-of-Safety of 1.4 (vs. 1.25 for EELV)

NASA human-rating Factor-of-Safety of 1.4 (vs. 1.25 for EELV)

Engine-out capability from release/lift-off

Engine-out capability from release/lift-off

Space Exploration Technologies Corporation 6Oct. 2, 2008

Fault tolerant avionicsFault tolerant avionics

Space Exploration Technologies Corporation 7Oct. 2, 2008

Completed all multi-engine test milestones Working up to full-duration 9-engine test

1-engine Nov 20,

2007

1-engine Nov 20,

2007

2-engineJan 18, 2008

2-engineJan 18, 2008

3-engine Mar 8, 2008

3-engine Mar 8, 2008

Run-tank liftAug 18,

2007

Run-tank liftAug 18,

2007

5-engine May 29,

2008

5-engine May 29,

2008

9-engine Aug 1, 2008

9-engine Aug 1, 2008

Demo C1, Q2 2009 – Core Functionality Only Very basic, up & back functionality

Tests fundamentals and puts an early success on the books

Demo C2, Q4 2009 – ISS Fly-By Approaches to within 10 km of ISS

Establishes command & telemetry cross-link

Demonstrates commanding by ISS crew

Demo C3, Q1 2010 – ISS Berthing ISS Proximity Operations, capture and berthing demo

Return cargo safely to Earth

Establishes system as operational

If funding for Crew Capability option is turned on in 2010:

Demo D1, 2011 – Unmanned high altitude abort

Demo D2, 2011 – Crew transport to ISS (three crew) Cargo mission will have proven ISS rendezvous and berthing

operations

A “light” flight crew (3) and minimal cargo to provide max delta-V and life support margins

Demo D3, 2012 – Crew transport to ISS (seven crew) Verifies ability to transport full complement of crew

Space Exploration Technologies Corporation 8Oct. 2, 2008

Ground swell of interest in Dragon amongst the following communities:

Biotech/biomedical research Flying on C2 Demo mission

Instrument & sensor developers Materials & space environments researchers Life sciences Microgravity research Radiation effects research Shuttle/ISS experimenters (without other

flight opportunities) Earth sciences (short-duration LEO missions) Sounding rocket community Space physics & relativity

Space Exploration Technologies Corporation 9Oct. 2, 2008 Image credit: NASA

We have customers interested in flying payloads on Dragon without going to ISS

Multi-manifesting opportunities

We have customers interested in flying payloads on Dragon without going to ISS

Multi-manifesting opportunities

Preliminary Design ReviewDemo-C3 Mission

Space Exploration Technologies Corporation 10Oct. 2, 2008 Image credit: NASA