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1 Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 Spaceflight – Small Payload Rideshare Conference 2015

Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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Page 1: Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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Systems Services Networks

SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna

June 9 2015

Spaceflight – Small Payload Rideshare Conference 2015

Page 2: Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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Spaceflight Industries includes three separate operating companies – Spaceflight Systems: Formerly Andrews Space – Founded in 1999 and producer

of small high performance spacecraft and components – Spaceflight Services: Founded in 2010 to provide launch services to the

emerging SmallSat community – Spaceflight Networks: Created in 2014 to provide communication services to

the emerging SmallSat community

Spaceflight Industries Introduction

Design Build Integrate Launch Operate

Systems Services Networks

Page 3: Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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Spaceflight Systems Introduction

SENTRY 1000[10cm x 10cm X-Section]

SENTRY 2000[20cm x 20cm X-Section]

SENTRY 4000[40cm x 46cm X-Section]

SCOUT 1 meter GSD Imaging Satellite (50kg)

We produce components, buses and spacecraft to enable high performance nanosat and microsat missions

Spacecraft Platforms (Buses) Fully Integrated Spacecraft

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Spaceflight Systems Product Overview

CORTEX Avionics

PYXIS Star Trackers

PYXIS CompassDual-camera, integrated rate

sensors, onboard processing unit

PYXIS TrackerSingle-camera,

lightweight, small form factor, remote

processing unit

Solar Arrays/ Batteries / Power Systems

CORTEX is a complete suite of small form factor avionics cards including a high-performance flight computer, power system,

instrumentation, communication and motor/valve drivers

Torque Rods

TQ-15 and TQ-40Magnetic torque rods,

redundant or non-redundant versions

*Licensed from Sinclair Interplanetary

216 W-Hr 7.2 Vdc Li-Ion battery20 W 6U solar arrays (single and dual string circuitry)

Custom Power Distribution Systems

Propulsion System

Warm-gas butane system offers up to 60 m/s deltaV and for 50 kg S/C

Page 5: Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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Average time from image capture to customer delivery

Spaceflight Networks Introduction

• Spaceflight provides turnkey communication data services to enable the emerging NanoSat / MicroSat / SmallSat market

– Deploying a global ground network that provides low and high bandwidth connectivity using UHF, S-band and X-band links

– Developing spacecraft radios that seamlessly integrate with this ground network to simplify spacecraft development and minimize operating costs for our customers

Dedicated antenna lease – 24/7 use of a single

antenna • S-/X-Band $50,000 per month • UHF $3,000 per month On Demand Access - Use of an antenna on an “as needed” basis to support your spacecraft mission • S-/X-Band $19.95 per minute • UHF $1.95 per minute

UHF antenna @ Seattle

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Spaceflight Services - Launch Summary

• Spaceflight provides turnkey launch solutions to enable the emerging NanoSat / MicroSat / SmallSat market

• Spaceflight has orbited 76 spacecraft

• We have another 115+ on contract to launch in the coming months / years

• First SHERPA mission manifested on a SpaceX F9 for Q4 2015 with 89 payloads on board

• Dedicated yearly cluster missions begin in Q3 2017 to LEO, 2018 for GTO

• Dedicated small launch vehicle capability available starting early 2017

Commercial rideshare cluster missions starting

in 2017

SHERPA rideshare accommodations and

in-orbit delivery starting in 2015

First payloads orbited in 2013

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Commercial Mission Pricing

• Spaceflight commercial pricing based on payload size and mass

• We arrange launches for secondary payloads ranging from CubeSats to MicroSats

• Commercial rideshare mission pricing from Low Earth Orbit to Low Lunar Orbit

Soyuz 2.1a / Bion-M1 Launch

Spaceflight is the ONLY rideshare provider to offer public commercial pricing

Containerized Satellite Class

Payload Type 3U 6U 12U 50 kg 100 kg 150 kg 200 kg 300 kg 450 kg* 750 kg* 1000 kg*

Length (cm) 34.05 34.05 34.05 80 100 100 100 125 200 300 350

Height/Dia (cm) 10.00 10.00 22.63 40 50 60 80 100 150 200 200

Width (cm) 10.00 22.63 22.63 40 50 60 80 100

Mass (kg) 5 10 20 50 100 150 200 300 450 750 1000 Price – LEO $295 $545 $995 $1,750 $3,950 $4,950 $5,950 $7,950 $17,500 $22,000 $28,000

Price – GTO $650 $995 $1,950 $3,250 $5,950 $6,950 $7,950 $9,950 CALL CALL CALL

Price - GSO/LLO $995 $1,990 $3,250 $6,500 $9,950 $12,950 $15,950 $19,900 CALL CALL CALL * Assume vertical integration with the Launch Vehicle where nominal diameter and length is given *** Priced in thousands. Specific mission pricing may vary

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SHERPA Overview

SHERPA 1st Flight – Q4 2015: • LEO SSO 10:30 LTDN • Up to 1265 kg of Secondary Payloads – 89

Spacecraft – Combination of 1U, 1.5U, 2U, 3U and 6U CubeSat

spacecraft – Three Microsatellites from 50 kg to 160 kg

• No Propulsion or Attitude Control

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SHERPA Accommodations: • 5 ports, each supporting up to 300 kg • Dimensions NTE 1m x 1m x 1.2m • Hosted Option for Power/Comm up to 3 years Future Capabilities: • 400 m/s Delta V for orbit change maneuvers • 1000 m/s Delta V from GTO for delivery to DRO • 2200 m/s Delta V from GTO to circularize up to 500kg payload in GSO

SHERPA is a hosted payload and in-space transportation solution that supports orbit raising and maneuvering of secondary payloads in low earth orbit, geosynchronous orbit placement,

low lunar orbit insertion, and interplanetary capability.

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SHERPA Adapters

Radial Port Adapter Supports 15” and 11.732” Separation Systems

Dual Port Adapter (2 <50kgs Satellites) Supports 11.732” and 8” Separation Systems

QuadPack Plate Supports 7 CubeSat Dispensers Currently Configured for ISIS QuadPacks

Hardware has arrived in Seattle

Page 10: Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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SHERPA Technical Details - Avionics

SHERPA is designed to fly as a stand alone system that is separated from the Launch Vehicle prior to initiation and completing the dispensing of the secondary spacecraft. The Avionics consist of a battery, flight computer, power distribution, radio and GPS system that relays telemetry data through the Spaceflight Network providing confirmation of separation and state vectors to the customer.

Internal view of the SHERPA Ports with the avionics system displayed.

Page 11: Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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SHERPA Adapters (continued)

Mechanical Fit Check of QuadPack Plate Adapters

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SHERPA-0 Fit Check

• Spaceflight has an experienced integration team. • Missions Managers Mitch Elson and Adam Hadaller performed SHERPA fit check

activities at Vandenberg in early March 2015

Spaceflight built volume simulators and performed a dry run integration

simulation to ensure the schedule timeline could be achieved and to

verify mechanical interfaces

SHERPA was successfully mated with the Launch Vehicle

Payload Attach Fitting and Primary Payload Adapter

Page 13: Systems Services Networks - SPRSA...Systems Services Networks SCOUT spacecraft Spaceflight’s First Launch Fairbanks Antenna June 9 2015 ... Created in 2014 to provide communication

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Mission Management Team

Peter Wegner - CTO Dr. Wegner has over twenty years of experience leading the development, deployment and operations of satellite and launch systems. Dr. Wegner was formerly the Director of the DoD’s Operationally Responsive Space Office, where he led an ~90 person staff of officers and civilians from the US Air Force, Army, Navy, Marines, and intelligence agencies with a $150M+ annual budget to develop and deliver space systems to meet urgent needs of the DoD in global operations.

Mitch Elson - Senior Engineer & Mission Manager Mr. Elson has 14 years of relevant experience as Military, Government Civilian and a DOD Systems Engineering and Technical Advisor (SETA). He served as an Air Force Officer from 2000 to 2004, working as a mission manager for space and target launch systems. Mr. Elson supported US Government organizations for another 10 years, most recently at the ORS Office. He served as a manager for the ORS-3 Minotaur I launch, integrating and successfully deploying 28 CubeSats. Adam Hadaller - Mission Manager Mr. Hadaller has lead launch campaigns at Spaceflight since 2012. Prior to working at Spaceflight, he served a four-year tour of duty with the United States Marine Corps as an infantryman. After the military, he completed a Bachelor of Science degree in Aeronautical and Astronautical engineering at the University of Washington. To date, he has successfully managed multiple launch campaigns to completion, with several more underway.

Kaitlyn Kelley - Mission Manager Ms. Kelley manages multiple Spaceflight launch campaigns for CubeSats and nanosatellites. She has experience with ISS deployment through Spaceflight partner, NanoRacks , and manages missions on the H-IIA and PSLV vehicles. Ms. Kelley earned bachelor's degrees in aerospace engineering and professional writing from Worcester Polytechnic Institute. She previously worked at Pratt & Whitney aircraft engines, supporting jet engine assembly and testing.

Alex Rawling - Mission Manager Mr. Rawling manages Soyuz launch campaigns and supports business development. He has DoD acquisition and project management experience having served for 7 years as an acquisition officer in the United States Air Force and as a launch mission manager for the ORS-1 mission, launched on a Minotaur. Mr. Rawling earned a bachelor's degree in Economics and Business from Virginia Military Institute.

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Spaceflight Cluster Mission – Q3 2017 – LEO SSO

Spaceflight purchases an entire LV and manifests two Co-Lead Customers who will determine launch schedule and orbit. Auxiliary payloads are aggregated to utilize excess

launch vehicle capacity

Secondary Customer – Business Class • Integrated on top of Dual Payload Carrier • Can influence orbital placement as long as Lead

Customer requirements are satisfied

Lead Customer – Microsatellite – First Class: • Integrated within Dual Payload Carrier • Determines launch campaign schedule & orbit

Orbits to LEO, GTO/HEO, and GSO

Auxiliary Satellites – Economy Class: • Integrated to Spaceflight’s SHERPA in-space tug • Max Mass – 300 kg per Port

550-600km SSO 10:30 LTDN Lead Customer Signed, Rideshare Cubesats and microsatellites signed Limited Capacity Remaining

Manifest Full

Limited Capacity

Limited Capacity

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2017A Cluster Mission CONOPS

Vandenberg Processing –

Seattle Processing

1

2

3

Over-the-Road Shipping

Hydrazine Fueling

L-30 Days L-10 Days

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Spaceflight Cluster Mission – Q1/Q2 2018 - GTO

Secondary Customer – Business Class • Integrated within Dual Payload Carrier

Lead Customer – GTO – First Class: • Comm spacecraft Integrated on top of Dual Payload

Carrier • Determines launch campaign schedule & orbit

Auxiliary Satellites – Economy Class: • Option for SHERPA 2200 to bring to geostationary orbit

Spaceflight purchases an entire LV and manifests two Co-Lead Customers who will determine launch schedule and orbit. Auxiliary payloads are aggregated to utilize excess

launch vehicle capacity

Nominal Orbit Parameters Perigee: 185 km - 600 km Apogee: 40,000 km - 110,000 km Inclination: 23° to 28.6° RAAN: TBD° Argument of Perigee: 180° +/- 10°