Eric Salwan Director of Commercial Business Development [email protected] FIREFLY | EVOLUTION AND ADDRESSABLE MARKETS
Specialized Cargo
Lunar Payload Reusability Lunar Orbit On-Orbit Refueling IoT / Small Sat Debris Mitigation Constellations De-Orbiting Multiple Inclinations Firefly will provide transformative orbital launchLunar Gatewayand Cargo in-space services -- from LEO to the moon -- to create Aggregated Expanded Missions Launchreliable, affordable and rapid access to space. Inclinations GEO Launch Medium / Large Dedicated Sat Dedicated Small Sat GTO Launch
$ Revenue Margin & $ Revenue Launch Launch
Constellation Replenishment
2020 2025
FireflyFirefly Aerospace, Aerospace, Inc. Inc. Proprietary Proprietary and and Confidential. Confidential FIREFLY | EVOLUTION AND ADDRESSABLE MARKETS
Specialized Cargo
Lunar Payload Reusability Lunar Orbit On-Orbit Refueling IoT / Small Sat Debris Mitigation Constellations De-Orbiting Multiple Inclinations Lunar Gateway Cargo
Aggregated Expanded Missions Launch Inclinations GEO Launch Medium / Large Dedicated Sat Dedicated Small Sat GTO Launch
$ Revenue Margin & $ Revenue Launch Launch
Constellation Replenishment
2020 2025
FireflyFirefly Aerospace, Aerospace, Inc. Inc. Proprietary Proprietary and and Confidential. Confidential MARKET | UNIQUELY POSITIONED
Cube Sat Small Sat Cube Sat LEO Small Sat LEO Small / Large Sat LEO LEO Lunar Manned Lunar Orbit Deep Space Cargo Spaceflight Dedicated Replenishment Dedicated Replenishment Constellation Constellation MEO GEO
Legend 1/4 2/4 3/4 4/4 LAUNCH VEHICLE | ALPHA FIREFLY | INTEGRATED STAGE TEST LAUNCH VEHICLE | ALPHA PROPULSION
o Proprietary, in-house propulsion o Based on US – Apollo & Shuttle heritage technology o Design simplified, leveraging modern manufacturing processes for optimal economics o Reaver – 1st Stage, 41,400 lb thrust – 4 engines o Lightning – 2nd Stage, 15,800 lb thrust – 1 engine o Lox/RP1 fuel o Lowest risk path o Highest performance for 1st stage o Single chamber, turbo-pump fed design o Regeneratively cooled o Unique tap-off cycle o Proprietary & patented ”crossfire” injector – industry leading performance, cost & simplicity o Proprietary turbopump design o Copper / nickel plated thrust chamber o Significant performance benefits vs. 3D printed Inconel o Design optimized for reusability – 100+ full missions per engine LAUNCH VEHICLE | ALPHA STRUCTURES
o All carbon composite structure o Optimal strength to weight / propellant mass fraction o Significant expertise and IP
o Materials, fabrics, resins and weaves o Automation & robotics and 3D printing o Superior volume production, greater consistency, reduced costs o Lower touch manufacturing than traditional aluminum structures o Unique capabilities o Linerless composite tanks o Cryogenic tolerances o Structures fully manufactured in-house o 25,000 sq foot composites assembly o Clean room facilities o Large-scale curing ovens o Significant “reusability” benefits o Strength o Water landing capacity ALPHA | COMPETITIVE PRICE POINT
YEAR OF MASS TO MASS TO ESTIMATED PRICE PER PRICE PER KG, VEHICLE OPERATOR FIRST LEO SSO PRICE PER KG, LEO SSO LAUNCH (kg) (kg) LAUNCH Terran Relativity 2021 1,250 900 $10M $8,000 $11,111 RS1 ABL Space Systems 2021 1,250 875 $12M $9,600 $13,714 Alpha Firefly 2020 1,000 630 $15M $15,000 $23,810 LauncherOne Virgin Orbit 2020 500 300 $12M $24,000 $40,000 Electron Rocket Lab 2018 225 150 $7.5M $33,333 $50,000 Kuaizhou 1A EXPACE 2017 380 200 $14.5M $38,158 $72,500 Minotaur 1 Orbital ATK 2000 600 350 $30M+ $50,000 $85,714 Pegasus XL Orbital ATK 1994 450 250 $36M $80,000 $144,000
*As of 9.1.2018 FIREFLY | TEAM
Senior Management
Ann Chinnery Brad Obrocto Robb Kulin Tom Markusic Mark Watt Brad Schneider Les Kovacs Shea Ferring Joel Waldrum Founder, CEO Vice President of Development Site Director of Director of Director of Engineering CFO (Acting) CRO Vice President of Business Development Mission Assurance Director Avionics Launch Operations
Sarah Hinze Eric Salwan Alona Kolisnyk John Courter Gary Lantz Adam Oakes John Cramer Brigette Oakes Deputy Program Manager Director of Commercial Director of International Director of Structures Director of Systems Director of Production Director of Test Director of Design & Business Development Business Development Engineering & Integration Analysis FIREFLY | ADVISORY BOARD
Jeff Bingham Terry Boardman James Cartwright Deborah James Jim Maser George Nield William F. Readdy
Majority Staff Director, Chief Engineer, Vice Chairman of the 23rd Secretary of Air Force, Senior Vice President, Associate Administrator Former Associate Administrator, U.S. Senate Committee Alliant Techsystems, Joint Chiefs of Staff, Department of Defense Aerojet Rocketdyne Federal Aviation NASA Office of Space Flight on Commerce, Science, Director of U.S. Department of Defense Space Business Unit Administration (FAA) and Transportation Space Launch Propulsion President, Vice Chairman, Commander, Science Applications Vice President, Manager, NASA Associate Administrator, Chief Engineer, U.S. Strategic Command International Corporation (SAIC) Pratt & Whitney Space Shuttle Program Flight International Space Station NASA, Office of Legislative Affairs Alliant Techsystems, Technical & Engineering Sector F135 Engine Program Integration Office Advisory Committee Shuttle Solid NASA Johnson Space Center Legislative Coordinator, Rocket Motor Program Director / Advisor, Astronaut, International Space Station Program Bain & Co, LeanIn.Org, Senior Scientist, STS-42, STS-51, STS-79 Unisys, Textron, Orbital Sciences Corporation MIT Lincoln Laboratory FACILITIES | ENGINEERING AND PRODUCTION
ENGINEERING FACILITIES PRODUCTION FACILITIES
o Austin Texas area (Cedar Park) o Firefly Aerospace possesses in-house capability to o 20k ft2 open-plan engineering facility fabricate all vehicle propulsion systems and structures o State-of-the-art analytical tools and o 5-axis CNC milling and turning metallics machine shop supercomputer computational resources o 30k ft2 composites fab shop o Mission Control to support remote participation in o Carbon fiber filament winding testing and launch activities o Clean room for composite layup o CMM and laser tracking systems o Avionics fab/test o Electroplating/surface finish shop FACILITIES | TEST AND LAUNCH
TEST FACILITIES LAUNCH FACILITIES
Test Site Aerial View
Horizontal Test Stand
Vertical Test Stand o Austin Texas area (Вriggs) o SLC-2W at Vandenberg Air Force Base o 200 acre test site with full utilities (water, 3-phase o Substantial existing infrastructure power, fiber-optic ethernet) o o Test Stand 1: engine/component test stand Polar & SSO launch inclinations o 150k lbf horizontal thrust stand o SLC-20 at Cape Canaveral Air Force Station o Test Stand 2: integrated stage test stand o Existing infrastructure o 150k lbf vertical test capability o Test Stand 3: Component Testing o Lunar launch inclinations o Test Stand 4: Structural Testing o Full stage compression and torsional loads FACILITIES | SCALE OPERATIONS
o Existing manufacturing capacity to MANUFACTURING manufacture 8 rockets per year o Alpha cadence of 24 launches per year in steady state o Plans to bring 200,000 sq ft manufacturing facility online in Florida in 2021 to meet steady state production demands o Break ground in 2020 NEW PROJECTS | ORBITAL TRANSFER VEHICLE
• In-space propulsive third stage • Ultra-efficient solar electric propulsion • Xenon / Hall Thrusters • Enables Alpha & Beta to perform advanced missions at venture-class launch costs • Orbit raising / lowering • GEO • Custom orbits for secondary payloads or constellations • Hosted payloads • Sustained super low altitude flight GENESIS | COMMERCIAL LUNAR PAYLOAD SERVICES
Commercial Lunar Payload Services (CLPS) • NASA contract to deliver robotic landers/rovers to surface of the Moon • Indefinite Duration Indefinite Quantity (IDIQ) contract • 14 winners…maximum contract value of $2.6B over 10 years Firefly Genesis Lunar Lander • Commercial version of IAI Beresheet Lunar Lander • Highest TRL commercial lunar lander • Firefly will propose Genesis mission for next small lander task order WHY FIREFLY | SERVICES AND CONVENIENCE
• Customized engineering services for complex mounting requirements • High fidelity analysis for accurate definition of loads and environments