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Corporate Motivations for Vertical Integration

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  • Quilty Analytics
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Corporate Motivations for Vertical Integration
A Parametric Assessment of Make vs. Buy Acquisition Approaches for Small Satellite Constellations
Caleb Williams
Space Systems Analyst
caleb.williams@spaceworks.aero | 770.379.8017
Co-authors: Jon Wallace, Bill Doncaster, & Jordan Shulman
Aug 2018
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Introduction to SpaceWorks
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Introduction to SpaceWorks | SEI Group
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Introduction to SpaceWorks | History in NASA Cost/Schedule Community
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Study Overview
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Study Overview | Corporate Motivations for Vertical Integration
Over the last 10 years, there has been a substantial shift in space industry attitudes towards
vertical integration, particularly in the small satellite sector
Unlike traditional GEO stationary satellite companies, small satellite companies are increasingly
choosing to manufacture, integrate, operate, and manage end user sales entirely in-house
Examples include Planet, Satellogic, and Capella Space
Recently, another shift has been observed: small satellite companies are further integrating
upstream into the development and manufacture of their own satellite components
SpaceWorks developed this study as an internal research effort aimed at better understanding
corporate motivations for the observed increase in vertical integration activity in the small
satellite sector
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COMPONENT MANUFACTURER
SYSTEM INTEGRATOR
OPERATOR
Study Overview | Vertical Integration in the Satellite Sector
Traditionally, satellite firms have solely operated spacecraft, but recently
they are additionally taking on manufacturer and integrator roles
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Study Overview | Investigative Approach
Three relevant motivations for vertical integration in the small satellite sector were identified
For each motivation the market scenario was quantitatively modeled using Galorath’s SEER-H
parametric costing tool to calculate the Average Per Unit Cost (APUC) and Theoretical First Unit
(TFU) cost for two different procurement approaches:
A “traditional” procurement approach in which the majority of the system is purchased from component
vendors (with the exception of the communications payload and system integration/test)
A “vertically integrated” procurement approach in which the manufacturer handles the entirety of the
development and manufacture of the satellite and components in-house
Two different satellite concepts were considered: a 3U communications CubeSat, and a 300 kg
communications Small Satellite (nominally for IOT and broadband applications)
Average Per Unit Cost (APUC) equals the sum of Research, Development,
Testing, & Evaluation and Production cost divided by total operational units
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Study Overview | Cases Considered
Motivations for Vertical Integration in the Small Satellite Sector
Baseline
Case
The baseline case
considers the impact of
overall constellation size on
corporate decisions to
vertically integrate. It uses
nominal market
assumptions to evaluate
whether constellation size
alone is enough to motivate
a satellite company to
vertically integrate. It also
serves as the basis for
additional case studies.
Case #1:
Market Power
Case study #1 examines
how market power may
influence the decision for
satellite companies to
vertically integrate.
Specifically, it takes into
account supplier/buyer
dynamics in each market
segment to evaluate
whether smart vendor
relations and negotiations
could change the decision
to vertically integrate.
Case #2:
Quality Control
Case study #2 looks into
how a desire for increased
quality control could lead a
firm to vertically integrate.
Unreliable components are
a common occurrence in
the small satellite industry,
and this case specifically
examines how different
reliability rates can motivate
satellite companies to
vertically integrate.
Case #3:
Vendor Disruptions
Case study #3 evaluates
how vendor disruptions can
increase transaction costs
and considers whether
vertical integration is a
viable alternative for
protecting a company’s
supply chain. It specifically
examines a scenario where
a vendor disruption for
CD&H and Power
subsystems occurs and
whether this could motivate
a firm to vertically integrate.
Market-Realistic
Case
The final case considers
each of the individual cases
in conjunction, applying the
lens of SpaceWorks’ market
expertise to model the most
realistic market scenario. It
specifically considers the
market differences between
the Cube Satellite and
Small Satellite segments
and applies them to
examine why firms in each
segment are vertically
integrating.
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Study Overview | Methodology
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Study Overview | Baseline Assumptions
All Cases Assumption 3U Cube Satellite 300 kg Satellite
Prototype Effort Low High
Learning Curve 85% Various (83% - 93%)1
Project Complexity Low Medium
Development Standard Commercial Commercial
Production Experience Medium High
Production Environment Medium Medium
Hardware Heritage Varying (COTS2Make) Varying (COTS2Make)
Prior Production Units Various (1 1000) Various (1 1000)
Market Power 50/50 50/50
Reliability 90% 97%
Vendor Disruptions None None
1 Learning Curve rates determined using Price Unit Learning Curve Framework
2COTS = Commercial off the Shelf
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Baseline Results
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$100k
$150k
$200k
$250k
$300k
$350k
$400k
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional Vertically Integrated
At more than 87
operational units
, vertical
integration is more
attractive in this segment,
but at the cost of more
upfront capital.
Constellation size alone
may
explain motivations
for vertical integration
in
this segment, as many
operators are targeting
fleets of 100+ satellites.
Baseline Results | 3U Cube Satellite
$10.6M
TFU
$1.6M
TFU
Vertically Integrated Baseline Traditional Baseline
(88, $195k)
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$5M
$7M
$8M
$10M
$11M
$13M
$14M
$16M
$17M
$19M
$20M
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Average Per Unit Cost
Number of Operational Satellites
Traditional Vertically Integrated
Baseline Results | 300 kg Small Satellite
TFU cost of the vertically
integrated approach in this
segment is 2x traditional
TFU (vs. 10x for the 3U
satellite), leading to a
lower breakeven point.
The vertically integrated
APUC curve is more
gradual in this segment
due to lower learning
improvements vs. the
CubeSat segment.
$239M
TFU
$114M
TFU
Vertically Integrated Baseline Traditional Baseline
(39, $11.3M)
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Case #1: Market Power
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A major motivation for vertical integration across all
sectors is to increase market power
SpaceWorks calculated the savings due to learning
effects and varied the supplier/buyer share of the
surplus to simulate the impact of market power
Surplus equals the value of the learning effect savings
Surplus is split evenly, in favor of the buyer, or in favor of
the or seller
Within the CubeSat segment, a large number of both
buyers and sellers has led to the ideal no one
dominates scenario (50/50 surplus split)
Within the 300 kg segment, relatively few buyers
combined with an influx of traditional GEO satellite
component suppliers have led to buyers dominating
(75/25 surplus split)
Case #1: Market Power | Framework & Methodology
Many
Few
One
One Few Many
High
Trading
Risk
Buyers
Dominate
Sellers
Dominate
No One
Dominates
Source: McKinsey & Company
Number of Buyers
Number of Sellers
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$100k
$150k
$200k
$250k
$300k
$350k
$400k
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional (25/75 Split) Traditional Baseline Vertically Integrated Baseline Traditional (75/25 Split)
Case #1: Market Power | 3U Cube Satellite
Market power has a
substantial impact on
constellation breakeven
and could be a compelling
reason to pursue vertical
integration.
Within the CubeSat
market, we currently have
a relatively balanced
distribution of buyers
and sellers, leading to
neither side dominating.
If there is a
shift in either
the number of buyers or
sellers (and thus market
power) in the future, this
could impact decisions to
vertically integrate.
$10.6M
TFU
$1.6M
TFU
Vertically Integrated Baseline Traditional Baseline
Traditional (25/75 Surplus Split) Traditional (75/25 Surplus Split)
(88, $195k)
(166, $134k)
(60, $252k)
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$5M
$7M
$8M
$10M
$11M
$13M
$14M
$16M
$17M
$19M
$20M
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional (25/75 Split) Traditional Baseline Vertically Integrated Baseline Traditional (75/25 Split)
Case #1: Market Power | 300 kg Small Satellite
In current market
conditions, companies will
find it easy to squeeze
suppliers
in this segment,
making vertical integration
less compelling.
Given the favorable market
conditions for buyers,
constellations up to 76
satellites are likely better
off using traditional
procurement approaches.
Companies must consider
expected market power
in the future, as well as
current trends to avoid a
mistaken decision to
vertically integrate.
$239M
TFU
$114M
TFU
Vertically Integrated Baseline Traditional Baseline
Traditional (25/75 Surplus Split) Traditional (75/25 Surplus Split)
(39, $11.3M)
(27, $14.7M)
(76, $8.2M)
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Case #2: Quality Control
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Case #2: Quality Control | Framework & Methodology
Improved quality control can also be a powerful
motivation for vertical integration, particularly in the
CubeSat segment, where many components are still
in their infancy
SpaceWorks calculated the total number of satellites
necessary for production to achieve a certain number
of operational satellites to simulate the cost impact of
different reliability rates
I.e., given a 90% reliability, to have 100 operational
satellites, 110 satellites would need to be produced vs. given
a 97% reliability, 103 satellites would need to be produced
Within the CubeSat segment, the baseline nominally
assumed a 90% reliability rate, but empirical evidence
suggests this may be closer to 70%
Within the 300 kg segment, more reliable components
and additional prototyping lead to increased reliability
nominally 97% for the baseline
Quicker
Design
Iterations
Increased
Production
Oversight
Streamlined
Component
Design
Vertically Integrated
Quality Control Benefits
Source: SpaceWorks Commercial
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$100k
$150k
$200k
$250k
$300k
$350k
$400k
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional (70% Reliability) Traditional Baseline Vertically Integrated Baseline Traditional (97% Reliability)
Case #2: Quality Control | 3U Cube Satellite
Moving from a low
reliability rate can be a
compelling reason to
integrate, but firms must
be able improve that
reliability in-house.
If satellites already have a
high reliability rate,
integrating to improve
incrementally is not
nearly as advantageous.
This particular analysis
does not consider the
potentially lost revenue
due to quality issue, which
could be substantial.
$10.6M
TFU
$1.6M
TFU
Vertically Integrated Baseline Traditional Baseline
Traditional (70% Reliability) Traditional (97% Reliability)
(88, $195k)
(67, $234k)
(99, $181k)
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$5M
$7M
$8M
$10M
$11M
$13M
$14M
$16M
$17M
$19M
$20M
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional (90% Reliability) Traditional Baseline Vertically Integrated Baseline Traditional (99% Reliability)
Case #2: Quality Control | 300 kg Small Satellite
Quality control in this
segment is not as
compelling of a motivation
for integration, as the
status-quo reliability is
already quite high.
Marginal improvements
in reliability yield
minimal change in
the constellation size
breakeven point.
Using new suppliers
and/or components may
result in lower TFU costs
,
but can also result in
lower reliability and a
different breakeven point.
$239M
TFU
$114M
TFU
Vertically Integrated Baseline Traditional Baseline
Traditional (90% Reliability) Traditional (99% Reliability)
(39, $11.3M)
(35, $12.6M)
(42, $11.1M)
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Case #3: Vendor Disruptions
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High transaction costs can result in a powerful
motivator for vertical integration
Typically satellite companies make a small number of
transactions for a large number of highly specialized
assets (resulting in low transaction costs)
The baseline case reflects this with zero vendor disruptions
Increased transaction costs would occur if, for
example, a supplier stopped selling a component,
and an additional vendor needed to be secured
SpaceWorks considered a supplier disruption for high
value subsystems (CD&H and Power) after the 16th
unit, forcing the manufacturer to find a new vendor
New subsystem development cost as well as a fractional
system development cost were factored in to account for
the higher transaction cost
Often
Seldom
Low High
Standardized
transactions (e.g.,
groceries)
Vertical integration
(e.g., bauxite,
specialized auto
components)
Detailed standardized
contracts (e.g., office
lease, credit sales
arrangements)
Detailed, probably
unique contract (e.g.,
major public
construction projects)
Asset Specificity, Durability, and Intensity
Transaction Frequency
Case #3: Vendor Disruptions | Framework & Methodology
Source: McKinsey & Company
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$100k
$150k
$200k
$250k
$300k
$350k
$400k
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional Baseline Vertically Integrated Baseline Power Supplier Disruption
CD&H Supplier Disruption Power & CD&H Supplier Disruption
Case #3: Vendor Disruptions | 3U Cube Satellite
Vendor disruptions have
minimal impact on
constellation breakeven
points, as their cost is
amortized across
satellites very quickly.
Concerns regarding
vendor
disruptions may be
overstated, leading to a
mistaken motivation for
vertical integration.
This analysis does not
consider if the
manufacturer brings the
component development
in-house, which could be
more costly.
$10.6M
TFU
$1.6M
TFU
Vertically Integrated Baseline Traditional Baseline
Power Supplier Disruption CD&H Supplier Disruption Power + CD&H Supplier Disruption
(88, $195k)
(86, $198k)
(87, $197kk)
(85, $200kk)
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$5M
$7M
$8M
$10M
$11M
$13M
$14M
$16M
$17M
$19M
$20M
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Vertically Integrated Baseline Power Supplier Disruption Traditional Baseline
CD&H Supplier Disruption Power & CD&H Supplier Disruption
Case #3: Vendor Disruptions | 300 kg Small Satellite
The impact of vendor
disruptions in this segment
is more substantial due
to more expensive
components, but it is still
overcome quickly.
The additional complexity
of components in this
segment may require
greater satellite
redesign, but
this was not
considered.
If additional subsystem
vendor disruptions
were to occur, there would
be more substantial
motivation for vertical
integration in this segment.
$239M
TFU
$114M
TFU
Vertically Integrated Baseline Traditional Baseline
Power Supplier Disruption CD&H Supplier Disruption Power + CD&H Supplier Disruption
(39, $11.3M)
(38, $11.8M)
(33, $12.8M)
(32, $13.1M)
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Integrating Market Expertise
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Final Results | Integrating Market Expertise
SpaceWorks has built significant insight into current market conditions and trends through
various forecasting and strategic analysis engagements with government and commercial clients
While each previous case considers various sensitivities to market conditions, they are evaluated
independent of one another
Integrating and evaluating the different sensitivities together based on current market trends gives
a glimpse into a “market-realistic” model for evaluating vertical integration decisions for small
satellite constellations
The final case considers only those conditions that are currently
observed in the market place for each segment
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$100k
$150k
$200k
$250k
$300k
$350k
$400k
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional (70% Reliability) Traditional Baseline Vertically Integrated Baseline
Final Results | 3U Cube Satellite
At 67 satellites
a vertically
integrated approach is
more cost-effective than
traditional manufacturing
for Cube Satellites.
In contrast
to the baseline,
the market-realistic 3U
model uses a 70%
reliability rate,
significantly lowering the
breakeven point.
The high TFU costs
associated with the
vertically integrated
approach provide insight
into why firms are not
adopting this approach.
$10.6M
TFU
$1.6M
TFU
(88, $195k)
(67, $234k)
Vertically Integrated (Realistic) Traditional (Realistic) Traditional (Initial Baseline)
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$5M
$7M
$8M
$10M
$11M
$13M
$14M
$16M
$17M
$19M
$20M
16 32 64 128 256
Average Per Unit Cost
Number of Operational Satellites
Traditional Baseline Vertically Integrated Baseline Traditional (75/25 Split)
Final Results | 300 kg Small Satellite
At 76 satellites, a
vertically integrated
approach becomes more
attractive than traditional
manufacturing approaches
in the 300 kg segment.
The constellation size
breakeven shifts
outward when considering
the current market
environment favoring
buyers in this segment.
Even in much larger
constellation sizes, the
benefits of vertical
integration are not as
drastic in this segment
as in the 3U segment.
$239M
TFU
$114M
TFU
Vertically Integrated (Realistic) Traditional (Realistic)
(39, $11.3M)
Vertically Integrated (Realistic) Traditional (Realistic) Traditional (Initial Baseline)
(76, $8.2M)
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Insights & Takeaways
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Insights & Takeaways | Conclusions
This analysis provides insight into real-world motivations for when and when not to vertically integrate
Applying market expertise has a dramatic impact on constellation-size breakeven points and helps to
illustrate why a venture such as IridiumNEXT (75 satellites) chose a traditional procurement
approach, while a venture like Spire (150+ satellites) is leveraging a vertically integrated approach
Of the cases considered, market power is the most compelling motivation for vertical integration
Within the Cube Satellite segment, market power is currently well balanced, thanks to a relatively large number of
both buyers and sellers, providing little insight into why manufacturers are integrating
Within the Small Satellite segment, market power is in currently heavily favor of the buyers, which demonstrate why
companies in this segment have been slower to adopt vertical integration strategies
Improved quality control, while often cited as a motivation for vertical integration, is compelling only when
large advancements in reliability can be achieved with a vertically integrated approach
Vendor disruptions are not a compelling reason for vertical integration as their cost is absorbed easily
by large-batch production runs
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Insights & Takeaways | Final Thoughts
Constellation size itself is likely the strongest motivator for vertical integration
Results indicate that manufacturers considering constellations greater than around 70 satellites in either
segment should be considering a vertically integrated approach
Despite the results presented here that indicate many of constellations currently in development
would benefit from vertical integration, such a strategy should be approached with caution
Vertical integration is a costly and near irreversible strategy with significant associated risks
The upfront investment costs (shown here as TFU costs) required for a vertically integrated approach offer
insight into why companies may not be pursuing this approach even given its advantages
The decision to vertically integrate should be made holistically, considering market expectations
in the future (not just current trends), and a variety of financial and organizational factors
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Insights & Takeaways | Future Research
Specific areas of future research identified by SpaceWorks include:
Consideration of additional satellite mass-classes and satellite application types
Consideration of additional types of vendor disruptions
Integration of more precise learning curve analysis for Cube Satellite components
Integration of revenue estimates and financial modeling (Net Present Value, Internal Rate of Return)
Evaluation of vertical integration decisions at the component-level
Evaluation of operator to manufacturer vertical integration
Evaluation of quasi-integration strategies (Joint Partnerships, Partial Vertical Integration)
… and many others
The current effort establishes a valuable baseline for understanding
motivations for vertical integration and opens many other lines of inquiry
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