Google Lunar XPrize Ofical Team SpaceMETA VIsion for MicroLaunch Market in 2016.

1. SpaceMETA
Material Interno

2. SpaceMETA by
IdeaValley & IdeaLabs
- Founded in
Petropolis in
Tecnopolo
Marambaia:

3. A Brief History …

4. SpaceMETA is a Oficial Team
participating on the Google
Lunar XPrize Race to land ,
survive 2 days and walk 500
Meters with a rover on the
Moon Surface.

5. A Lot of Ideas for the Primary Brasil Lunar Mission
SpaceMETA Goals
- Mission Profile:
Launch the 3 Balls
using Balloon+Ethanol
Engine or Cyclone 4.
( Agreement Signed )
- Focus on Innovation (
Robotics, Ideas,
Special Partnership
with market players
and 5 Years on
SoftWare development
)
- Landing Zone: Mare
Nectaris ( T.B.C )
- Prize Goals: 500 Mts ,
Surviver , Water
- Not Solved Yeat: Soft
Landing , Plate
Payload Delivery ,
Transmission.
- Orbit Details …

6. Confidential & Proprietary
Around the World
SpaceMETA

7. Washington
Sillicon Valley - Google
Budapest Chile
Tokyo
BRASIL

8. Confidential & Proprietary
SpaceMETA Lunar Rover
SOLITAIRE

9. SOLITAIRE
Multipurpose Rover with Fault Tolerant Long Motion

10. Confidential & Proprietary
A Huge Midia Opportunity
SpaceMETA

11. A Huge Good Midia Opportunity

12. Confidential & Proprietary
The new Space Market Opportunity
SpaceMETA

13. The
Exponencial
Growth
Of
Technology
2020

14. Confidential & Proprietary
The MicroLaunch Market
SpaceMETA

15. SpaceMETA.
Market
Evolution
2015
2.000.000 Kg 20 Kg
40 Units/Year 1000 Units/Year
Traditional MicroSat
4 Years Dev 3 Months Dev
100 USM Launch 2 USM Launch
4 US Bi Mkt Size / year 2Bi Mkt Size / Year
5 Kg / 3-5 Mts Resolution2.000 Kg / 15-100 Mts
2010
200 US Bi ( 2013)

16. SpaceMETA.
Satelite
Market
Scenario
200 US Bi ( 2013)
Mkt Share Meteo
Mil
Scien
Com Comm
Nav
R&D
Mkt Segment Launch
Manufac
Services
Ground Equip
Orbit MEO
GEO
Near GEO
LEO
CubeSats

17. Confidential & Proprietary
Business Model Strategy
SpaceMETA

18. SpaceMETA.
Business
Model
Strategy
Planning and Simulation
Building Key Parts
Launch
And
Recovery
Enable
Internet
APIs

19. MISSION STRUCTURE PRELIMINARY DEFINITION

20. Missão Alfa Missao Beta Missao Teta
Launch Data
Objetivo: Jump Start
Prazo : 3 Meses = TBD
Mission Profile: Elevar uma carga
de 2 KG acima da zona de Karman,
com tecnologia hibrida, telemetria
completa com imagem e
recuperacao diferenciada.
Orçamento:
Diretor da Missao:
Diretor de Voo:
KPI:
Launch Data
Objetivo: Technologycal
Prazo : 6 Meses
Mission Profile: Elevar uma carga
de 2 KG acima em espaço orbital,
com tecnologia hibrida, telemetria
completa com imagem e
recuperacao diferenciada.
Orçamento:
Diretor da Missao:
Diretor de Voo:
KPI:
Launch Data
Objetivo: Moon Landing
Prazo : 12 Meses
Mission Profile: Transportar uma
carga de 5 Kg ate a superficie da
Lua.
Orçamento:
Diretor da Missao:
Diretor de Voo:
KPI:

21. Confidential & Proprietary
POWER PROFILE
- Margin of
Success
- TBD
- I - Identification of the range of the
landing site window.
- II - Ballistic Routing Module of the
landing site.
- III - Descent Control.
(A) Take Off
TBD:
(B) First Stage
TBD
(C) Second Stage
TBD
(D) Firing
I - Calculation of lunar trajectory.
II - Vector Pointing to the target.
III - Speed gain calculation
The margin of sucess accepts a considerable
variation in speed, altitude and position. Within the
limits checked in the model.
(G) Recovering
TBD
(E) landing Aproach
TBD
(F) MISSION CONCLUSION KPI
TBD
Missao Alfa

22. Confidential & Proprietary
POWER PROFILE
- Margin of
Success
- TBD
- I - Identification of the range of the
landing site window.
- II - Ballistic Routing Module of the
landing site.
- III - Descent Control.
(A) Take Off
TBD:
(B) First Stage
TBD
(C) Second Stage
TBD
(D) Firing
I - Calculation of lunar trajectory.
II - Vector Pointing to the target.
III - Speed gain calculation
The margin of sucess accepts a considerable
variation in speed, altitude and position. Within the
limits checked in the model.
(G) Recovering
TBD
(E) landing Aproach
TBD
(F) MISSION CONCLUSION KPI
TBD
Missao BETA

23. Confidential & Proprietary
POWER PROFILE
- Margin of
Success: It accepts a
considerable variation in speed, altitude
and position. Within the limits checked
in the model.
- I - Identification of the range of the
landing site window.
- II - Ballistic Routing Module of the
landing site.
- III - Descent Control.
(A) First Stage
Aceleração: 4.5G/s [0, 116](s)
Massa: 198.033Kg
Propellant consumption: 445Kg/s
Velocity: [0,1,223.837]Km/s
Altitude em 132(s): ~=43,346Km:
(B) Second Stage
Aceleração: 6.8G/s [129, 282](s)
Mass: 68,614.7Kg
Propellant consumption: 45Kg/s
Velocity: [1,223.837,
4,372.468]Km/s
Altitude em 300(s): ~=135Km
(C) Third Stage
Aceleração: 3.4G/s
Time: [292, 1,080](s)
Massa: 14,110.3Kg
Propellant consumption: 7.76Kg/s
Velocity limit: 7,78Km/s
Altitude em 1,568(s): ~=
2,188.686Km
(D) Launch Ballistic
I - Calculation of lunar trajectory.
II - Vector Pointing to the target.
III - Speed gain calculation
The margin of sucess accepts a considerable
variation in speed, altitude and position. Within the
limits checked in the model.
(G) Landing Module
I - Identification of the range of
the landing site window.
II - Ballistic Routing module of the
landing site.
III - Descent control.
(E) Lunar Approach
Distance from the lunar center: <10,000km
Speed of arrival, ~ = 12K / s.
Deceleration rate:
Sprint speed:
End distance from CL:
(F) Adaptive Entering Orbit
The solution is obtained through a congruence
of the states of displacement vectors and other
magnitudes.
Missao Teta

24. Confidential & Proprietary
Action Plan
SpaceMETA

25. Action Plan
• 12 Months to Land a rover on the Moon
• Fundraise 3 USM to sponsor R&D and First Rocket Building and First Laucnh
in Brasil Soil
• Federal PPP With Alcantara with 1.5% Brute Royaltie by the License of Installations
• Joint Venture for Tech Transfer with International Partners , subjected to
Brazilian Congress Aproval
• Involvment of Brasil armys to suport logistics
( Rocket transportation and security )
• Creation of a complete high tech suply chain for thew microsatelite market

26. Confidential & Proprietary
Thank
You

27. • 1
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• 3
• 1
• 2
• 3
• 1
• 2
• 3
StakeHolder Missao Alfa
StakeHolder Porque Interesse
Principal
A Matriz de StakeHolder Compelta esta no Google Drive do Projeto

28. Confidential & Proprietary
SPACEMETA
THANK YOU.

30. SpaceMET
A
Executive
Summary
Missao ALFA
• INTRO
• How we will do It
• Why it is important
• R&D road Map
• Financial Opportunity
• Return

31. Confidential & Proprietary
QA
• At Least one physical event in the Teams Coutry
• Focus Should be on the entrepreneurs , not in the Sponsors
• Entrepreneurs in this high risk venture should be placed in the
history , at least by the courage for the try
• Accelerate the Space EcoSystems conecting people and
bringing venture capital to the pure innovative idea

32. The Space Market to SpaceMETA

33. • We are here to do the Impossible things today ,,,
the possible ones the nature will do alone
tomorrow. – Sergio / SpaceMETA

35. Confidential & Proprietary
SpaceMETA
Sergio Cabral
Cavalcanti

36. Confidential & Proprietary
SpaceMETA
Sergio Cabral Cavalcanti

37. Content
Confidential & Proprietary
TITLE

38. Type content here.
Confidential & Proprietary

39. Confidential & Proprietary
ceMETA
ank You

40. Confidential & Proprietary
SpaceMETA
Obrigado

41. SpaceMETA.
Sergio
Cabral
Cavalcanti.