This is a presentation peformed by Sergio Cabral Cavalcanti from SpaceMETA realized in Tokyo in 2015 by Google Lunar XPrize with Goals to Land a Robot in the Moon Surface With Spacecial thanks from Edge of Space and CropCircles.

1. SpaceMETA
Sergio Cabral Cavalcanti
こんにちは

2. SpaceMETA by
IdeaValley & IdeaLabs
- Team Leader:
Sergio Cabral
Cavalcanti
- Total Members: 50
- Dedicated to
SpaceMETA: 10%
- Major Sponsors:
CRJ , IdeaGroup ,
Intel , Family and
Friends, SM Family.
CropCircles,
- Phase 1-Key
People: Sergio ,
Rafael , Marcos
Tulio , AntMaper,
Juliana , Chico ,
Dominique
- Operations:
Rio de Janeiro ,
Sao Paulo , Brasilia
, Alcantara.

3. A Brief History …

5. 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. SOLITAIRE
Multipurpose Rover with Long Motion

7. Mission Orbit Profile

8. 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.

9. Earth Atmosphere Moon
Launch Data
March 2016 Full Monn 00:40PM
*(Meio-Dia)
Diameter X,Y,Z: = (12.742, 12.713 , 12.742)
Inclinação perpendicular a
eclíptica: 23 ° 26’ 21’’
Velocidade de Rotação:~= 500 m/s.
Mass: 5,972 × 10
24 kg
Visibility: Still 36Km Alt
Temperatura, Pressão e
Densidade
• International Standard
Atmosphere
Drag:
Dist: 356.720
Diameter 3,474.810Km
Velocidade: ~= 1,080K/s
Massa:7.3431 × 1022
lInclinação em relação a ecliptica: 5°9’
Landing Zone: Mar do Néctar

10. Earth Atmosphere Moon
Launch Data
March 2016 Full Monn 00:40PM
*(Meio-Dia)
Diameter X,Y,Z: = (12.742, 12.713 , 12.742)
Inclinação perpendicular a
eclíptica: 23 ° 26’ 21’’
Velocidade de Rotação:~= 500 m/s.
Mass: 5,972 × 10
24 kg
Visibility: Still 36Km Alt
Temperatura, Pressão e
Densidade
• International Standard
Atmosphere
Drag:
Dist: 356.720
Diameter 3,474.810Km
Velocidade: ~= 1,080K/s
Massa:7.3431 × 1022
lInclinação em relação a ecliptica: 5°9’
Landing Zone: Mar do Néctar

11. SpaceMETA MileStones Step Level Knowladge Economical Report
• Launch Agreement –
done – pre-concluded
• Moon/Mars Rovers –
pre-conclude and in
POC programmed in
SPICES Hawaii
• Mission Orbit SW and
Methodology -
Concluded
• Giant Inflatable
Anthenas – POC in
North of Brasil Desert
• Political Sector Issues
• MTA Compliance
• Soft Landing/Payload
• Kick Motors
• Communications
• Heat Transfer
• Be Green
• Outerspace Fuels
• Intel Sponsorship
• IdeaLabs Seed Capital
• 1 USD Risk Capital
• 10 USD Private / ROI
• F&F
• Big Industry players
intent to participate
STATUS REPORT

12. Confidential & Proprietary
How to Increment Teams Support
• 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

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

16. Confidential & Proprietary
SPACEMETA
THANK YOU.

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SpaceMETA
Sergio Cabral
Cavalcanti

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SpaceMETA
Sergio Cabral Cavalcanti

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ceMETA
ank You

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SpaceMETA
Obrigado

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Sergio
Cabral
Cavalcanti.

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A
Sergio Cabral
Cavalcanti.

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THANK YOU.