A copy of the business plan in the SAN Foundation.

1. Alexander Mayboroda
AVANTA сonsulting
Solar Energy and Space
Transportation System
Orbitron
2016

2. Global energy market
• Decision of financing programs of development of solar andDecision of financing programs of development of solar and
other alternative energy sources was concluded on the UNother alternative energy sources was concluded on the UN
climate conference in Paris 2015.climate conference in Paris 2015.
• By the year 2020 the Green Climate Fund must achieveBy the year 2020 the Green Climate Fund must achieve
expanses of 100 billion dollars per year to make transition toexpanses of 100 billion dollars per year to make transition to
ecologically cleaner sources.ecologically cleaner sources.

3. Global energy market
• Minimal demand for all kinds of equipment forMinimal demand for all kinds of equipment for
global energy - 12,2 trillion dollars for period ofglobal energy - 12,2 trillion dollars for period of
the year 2013 to 2033.the year 2013 to 2033.
• On average it is 718 billion dollars per year.On average it is 718 billion dollars per year.

4. Semiconductor market of space
manufacturing
• Segment of the world market in form of photoelectric
converters exceeds 100 billion dollars per year.
• Thin-membrane solar batteries can be produced on orbital
spacecraft «OKA-T» according to technologies of the
Institute of semiconductor physics, Siberian branch of the
Russian Academy of Sciences and the University of
Houston USA. 4

5. Semiconductor market of space
manufacturing
• Technological orbital spacecraft «OKA-T» uses high vacuum in a
wake zone for manufacturing thin-membrane solar battery.
• Manufacturing process in «OKA-T» will be cheaper than on a land,
provided with price reduction of materials delivery up to 3000 dollars
per kilogram (from the current level of 40 thousand dollars).
5

6. Market of equipment for solar energy with
elements of space base
• Future of solar energy - solar satellite power stations.
• Satellite solar power stations are 6-15 times more effective than land solar power
stations.
• Due to growth of electric cars sales, market of energy equipment may grow from
0,7 trillion dollars per year, up to 3,5 trillion dollars per year.
• Solar power stations require cargo extravehicular excursion prices in a range of
100-200 dollars per kilogram (1000 dollars per kilogram in startup period) .
• However at the present time the range of prices is 10-50 thousand dollars per
kilogram.

7. Market of equipment for solar energy with
elements of space basing
• Energy supply of sea and air vessels from solar satellite power stationsEnergy supply of sea and air vessels from solar satellite power stations
creates additional demands for equipment for 0,3-0,5 trillion dollars percreates additional demands for equipment for 0,3-0,5 trillion dollars per
year.year.
• Replacement of modern cars using internal combustion engines byReplacement of modern cars using internal combustion engines by
electric cars creates demand for additional power, which 5-10 exceedselectric cars creates demand for additional power, which 5-10 exceeds
attained power plant capacities, which in perspective provides additionalattained power plant capacities, which in perspective provides additional
demand at an amount of 3-7 trillion dollars per year.demand at an amount of 3-7 trillion dollars per year.

8. Material market for space manufacturing
• Demand for cheap delivery of rocket fuel components to orbital stations
exists, as well as demand for aluminum, titan, nickel, carbon, silicon and
other materials, which are necessary for manufacturing components and
space satellite drones under the program AMAZE.
• Demand for space manufacturing of spacecrafts reaches up to 17 billion
dollars per years, for fuel production - 5 billion dollars per year.
• European space agency accepted AMAZE program: implementation of
3D-printing for creation of metal parts and components of spacecrafts,
aircrafts and thermonuclear reactors.
• European space agency invested over 20 million euro into the research
of the creation of "Methods of three-dimensional print AMAZE".
8

9. SPS "Orbitron" - pricing task solution
• Space transportation system "Orbitron" - transport with
delivery prime cost of 50-250 dollars per kilogram.
• Commercial price will be 250-1000 dollars per kilogram.
• System "Orbitron" is recognized as WIPO invention, having
world novelty and industrial applicability, it is based on
tested technologies and devices.

10. Prototypes of the system "Orbitron"
• VKSN - soviet prototype of the
system "Orbitron"
• VKSN or ASPC - aerospace plane
with accumulation (of oxygen).
• Contributor VKSN (ASPC)
academician of Russian Academy
of Science Marov, M. Y.
• PROFAC – foreign prototype of
the system "Orbitron"
• PROFAC – Propulsive Fluid
Accumulator.
•
• VKSN-PROFAC were
successfully solving price tasks.

11. Prototypes of the system "Orbitron"
• Prototypes ASPC -PROFAC are airborne spacecrafts,
which orbit at altitude of 100-120 kilometers, on a border
of atmosphere and space.
• ASPC -PROFAC are equipped with air diffusers, same
as with uniflow engines of hypersonic aircrafts, which
capture discharged air.
• Entrapped air is liquefied: oxygen accumulates; nitrogen
enters into electric motor to create a reactive jet. 11

12. Prototypes of the system "Orbitron"
• Airborne spacecrafts like ASPC-PROFAC during flight in
relatively dense layers of atmosphere (100-120
kilometers) couldn't use solar panels due to their "sail
effect"
• Therefore a nuclear reactor had to supply engines with
energy.
• Due to international agreement on prohibition of nuclear
spacecraft flights at altitudes below 800 kilometers, a very
promising project BKCH-PROFAC was shut down. 12

13. The system "Orbitron"
• Orbital collector of the system "Orbitron" doesn't have prohibited nuclear
reactor onboard, because it can use solar panels due to high orbit altitude
(from 280 kilometers) and solar panels fold at lower altitudes.
• Removal of nuclear reactor cancels the ban on usage of highly efficient
systems ASPC-PROFAC.
• High altitude of orbital collector provides that required concentration of gas
on a flight path of collector is created artificially, with a help of suborbital
reusable rockets that lift gas gasholders-ballonets systems with necessary
gases.
• Orbital collector (with folded solar panels) passes through ballonet
systems and gathers gas.

14. The system "Orbitron"
• Orbital collector of the system "Orbitron" differs from prototypes VKCH
-PROFAC, thanks to the flow of gases not from the atmosphere, it can
receive almost any substances, not only oxygen and nitrogen.
• Thus at a price of 99% below normal, hydrocarbons and other required
substances can be delivered to production spacecrafts, for manufacturing
technical products and rocket fuel in space.
• Similarly metals can be supplied, as well as silicon and semiconductor
components of manufacturing, for example, gases such: iron pentacarbonyl,
cobalt hydrocarbonyl, nickel carbonyl, tungsten hexafluoride and uranium,
hydrogen compounds of silicon, germanium, tin, lead, borum.

15. The system "Orbitron"
• From prototypes of STS the "Orbitron"
differs in horizontal gas column,
absorbed by collector, artificially
created at height of its orbit.
• Ballonets are used for this because of
a high-durable membrane (UHMWPE)
with an ultimate toughness of 1-2
Gigapascals in a form of a sleeve
(cylinder) with a length from 100 to
1000 meters.
• Collector with folded solar panels
passes through a ballonet and
captures a portion of a contained gas.
• The ballonets are raised by suborbital
carrier-rocket at any desired height.
• Consequently, thanks to orbits
altitude, conditions of using solar
panels instead of a nuclear reactor
are provided.
15

16. The system "Orbitron"
• The system "Orbitron"
• STS "Orbitron" consists of two parts:
• the first part - aerospace (land-based) on a basis
of suborbital rockets (launch numbers from 200
to 500);
• the second part - orbital, representing a satellite-
collector of cargo, such SC PROFAC.
• Aerospace part is intended for creation of gas-
filled channel "runway" on a path in front of an
orbit collector, with "track" of a high
concentration of matter (0.01 to 0.1 kilograms/
square meter), compared to others in airless
space.
• For creation of a gas canal, cylindrical bags
made of high-strength thin-membrane material
are used.
• Recovery of kinetic energy reserves of a collector
is conducted by operating low-thrust engines, for
example, electric propulsion engines with a
specific impulse of 16-32 kilometer/second. 16

17. The system "Orbitron"
Video-schemes to the project "Orbitron":
• https://youtu.be/EDSin1hL6dY
• https://youtu.be/q1uoNl6st_g

18. The system "Orbitron"
• Using the potential and kinetic energy of the regolith for the
accumulation of oxygen and nitrogen from the atmosphere.
• Mass of the captured gas is equal to 40% of the mass of regolith.
• Nitrogen is combined with magnesium, calcium or lithium is used as a
propellant for flights to asteroids.

19. The transport complex "Orbitron"
• The system "Orbitron" includes:
orbital collector of gases;
orbital fuel depot;
spacecraft-refueler;
reusable suborbital rockets;
ground-based launchers.
• In conjunction with other systems, a transport complex "Orbitron" is formed, which
includes: reusable orbital tug for withdrawal of artificial earth satellite
ongeostationary orbit;
reusable orbital multistage rockets;
space platform for hosting 3D printers;
chemical engineering module for substances processing,
which were accumulated by a collector, in order to obtain materials for
3D-printers;
power module with fiber-optic lasers with direct solar absorption for energy
supply of collectors motors.
• The mass of the orbital collector is 3600 kg, its engines electric power is 600
kilowatts (on the first stage).
• Suborbital rockets have mass of 2000 kilograms and load capacity varying from
10 kilograms to 200 kilograms. 19

20. The transport complex "Orbitron"
• The basis of the complex - orbital fuel depot, which provides
refueling of spacecrafts with cheap rocket fuel and,
consequently, multi usage of rocket technology.
• Refilling of interorbital tug provides its return from
geostationary orbit and further reuse (25-50 times).
• Refilling of a second (orbital) stage of a carrier rocket, after
delivery of cargo into orbit, provides damping of orbital
velocity and, consequently, subsequent return to Earth for
reuse (10-25), in addition to reusability of the first stage of
Falcon type.
• Space platforms with 3D-printers, in addition to components
of space power plants, produces heat shields and capsules
from inexpensive materials in order to achieve return of
interorbital tugs on stationary orbit and rocket stages from
orbit to Earth. 20

21. Patents
• Method and system for delivering cargoes into space. US 8882047 B2.
Status: Grant of patent is intended
• Method for delivering cargoes into space and a system for implementation of same.
EP2390188 Status: Grant of patent is intended (Great Britain, Germany, France).
• Способ доставки грузов в космос и система его осуществления.
Patent of Russia RU2398717
• Способ доставки грузов в космос и система его осуществления.
Patent of Eurasia Patent Organization 017577
• Спосіб доставки вантажів в космос і система його здійснення.
Patent of the Ukraine 99230
• Способ энергообеспечения космических аппаратов-накопителей.
Patent of Russia RU2451631
• Energy supply method for spacecrafts-accumulators.
Patent application pending US 2013/0233974 A1
• Method and system for feeding jet engines.
Patent application pending US 2014/0326832 A1
21

22. Patents
22mayboro@gmail.comwww.mayboroda.com

23. Business model
• Reduce up to 99% of transportation costs on space manufacturing,
provides prices, advantageous for customers, and greater margin to a
service provider.
• The buyers: the energy concern RWE, State Grid and ACWA Power;
company DEWA; the developers of extraterrestrial mineral resources,
Planetary Resources, Deep Space Industries and Innovative Advanced
Concepts; national aerospace agencies.
• Services: delivery of materials into space for 3D printers and modules for
the type OKA-T; delivery of rocket fuel to orbital depots; development of
solar energy with space-based elements.

24. Orbitron Team
• Idea of the Project: Alexander MayborodaIdea of the Project: Alexander Mayboroda
• Project Manager: Vladimir MigelProject Manager: Vladimir Migel
• Leading Specialists:Leading Specialists:
D.K. Dragun, V.M. Melnikov, O.P. Pchelyakov, V.I. Florov.D.K. Dragun, V.M. Melnikov, O.P. Pchelyakov, V.I. Florov.
• They have experience of international project managers on the orbitalThey have experience of international project managers on the orbital
stations.stations.
• Main participants and their skills: the team has ten specialists withMain participants and their skills: the team has ten specialists with
necessary qualifications, knowledge and specialists with necessarynecessary qualifications, knowledge and specialists with necessary
qualifications, knowledge and experience.qualifications, knowledge and experience.
• Among them, there are specialists of TSNIIMASH, Vympel DesignAmong them, there are specialists of TSNIIMASH, Vympel Design
Engineering Department, Moscow State Technical University namedEngineering Department, Moscow State Technical University named
after N.E. Bauman, Space Research Institute of Russian Academyafterafter N.E. Bauman, Space Research Institute of Russian Academyafter
N.E. Bauman, Space Research Institute of Russian Academy ofN.E. Bauman, Space Research Institute of Russian Academy of
Sciences, Institute of Semiconductor Physics of Siberian Department ofSciences, Institute of Semiconductor Physics of Siberian Department of
Russian Academy of Sciences, Sputniks Company.Russian Academy of Sciences, Sputniks Company. 24

25. Orbitron Team
25
Vladimir Migel Alexander Mayboroda
Dmitry Dragun
Vitaly Melnikov
Oleg Pchelyakov

26. Orbitron Team
26
Vadim FlorovVadim Florov
Alexander Popov
Denis Anisimov
Yury Lebedev
Victor Korovin
Archie DevdarianiArchie Devdariani

27. Current status and schedule
• As for 2016: presence of intellectual property for technology "Orbitron" in the
USA, EU, CIS; negotiations with foreign investors and potential business
partners; opening of branch establishment in the US and the EU.
• Year 2016: creation of a multinational energy corporation based AVANTA-
consulting, companies in the U.S. and the EU, owning individual
technological components that are important for the implementation of the
system "Orbitron", transition from scientific research to experimental design
works, production of demo sub-orbital and orbital subsystems, test bench
tests, obtainment of additional "umbrella patents".
• Year 2017: demonstration tests of samples in space.
• Year 2019: completion of R&D and scale up of the project, deployment of
orbital retranslators of energy and space-based solar power-based system
"Orbitron", orbital systems OKA-T with space 3D-printers for the production
of solar batteries, and additional issue of shares.
• Year 2021: the output of the system to cost-effective operating mode, and
additional issue of shares.
• Year 2030: achieving 15 percent of installed power capacity of space
stations from current needs of updating global fund electricity power
generation (gross revenue of 100 billion dollars per year).
• Year 2036: achieving 30 percent of total sales of equipment for global
energy industry (gross income of 200 billion dollars per year).

28. Needs for investments
• 2016 – 0.4 million dollars.
• 2017 – 1.0 million dollars.
• 2018 – 2.6 million dollars.
• 2019 – 36 million dollars - attracting additional investment.
• 2020 – 82 million dollars - attracting additional investment
(plus 30 million dollars in a form of advance payments for
transport services at first 6-7 months after the launch of
the "Orbitron" exploitation).
• In 2020, sales of shares and receipt of founders profit of
818 million dollars.
• The cost of creating the system is 112 million dollars.
• In the period from 2020 to 2030 gross income –
• 3.13 billion dollars, profit - 2.38 billion dollars.
28

29. Cap Table
• The investor No. 1: AVANTA-consulting, shares (60%)
60 million dollars. USA (Intellectual Property).
• Investor No. 2: GCF and related funds, stocks (40%)
40 million dollars. USA.
• After additional share issue (in the year 2020) and reinvestment of
part of promoters profits in fund of the corporation, capitalization table
(Capitalization table) takes the following form:
• The investor No. 1:
AVANTA-consulting, shares (55,08%) 550,8 million dollars. USA.
• Investor No. 2:
GCF and related funds, shares (36,72%) 367,2 million dollars.
USA.
• The investor No. 3:
Minority shareholders, of shares (8,2%) 82 million dollars. USA.
29

30. Contact information
• Address: 150 Bolshaya Sadovaya St., office 909,
Rostov-on-Don, 344000, Russia.
• Tel.: +7 (863) 221 73 71, +7 (863) 263 32 94
• E-mail: mayboroda@avanta-consulting.ru
• Web-site: www.mayboroda.com
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31. Thank you for your attention
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