SlideShare una empresa de Scribd logo
1 de 33
44 PASSENGERS + 4 P/L’s SUB-ORBITAL
REUSABLE BLASTING SURVIVAL
VEHICLE
22 October 2014 – Naples Conference: «How to create jobs with the new Aerospace Industry»
S/S Equipment
bay
Light weight
shock-absorber
Fairing made up by
Carbon Fibre (CFRP)
sandwich panels
Pod Equipment
bay
(parachutes,
batteries,
tanks,...)
Light weight
shock-absorber
Cone pyro-separation detail
Panel for S/S
Equipment in the most
protected area
The Pod
•Typical accomodation of 4 Passengers
•It is the only pressurized part of the SHIPINSPACE
vehicle
•Seat design tailored to extra large people having
seats width of 650 mm against the 450 typical of
an economic class.
•Seats are designed in such a way Passengers can
withstand lateral loads (0,5g)
•Seats packaging can rotate along the axis normal
to the window
S/S’s volume
(unpressurized)
The Pod
The internal configuration (shown in this artistic view) will have COSMO-like internal wall painting with small
led providing a unique suggestion scenario. Passengers will have the impression to be in a continuous media
with the outside view. Mission screen with major parameters will be embedded in a seat packaging arm.
View of the Passengers close to the window
The 800 mm
diameter window, 7
times larger than a
wide-body Aircraft
one, will permit an
outstanding view of
outside even for
the 2 Passengers
close to the
window.
During the 6 min of
0-g the
Passengers can
move freely inside
the Module getting
their preferred
outside picture
View of the Passengers located far from the hatch port
During the 6 min of 0-g at the top of the Parabolic flight Passengers experience weightlessness in free flying
inside the Pod. An ergonomic study could verify that the space around the Passengers is higher than that of a
business class of a wide-body aircraft
Mission details
Slight rotation along Z axis to let
Passengers having the same view
Manoeuvering phase
Landing phase
Passengers configuration during descent and landing
The loads during
the descent are
normal to this
figure plane.
The Pods in the
2° floor and in the
middle have only
2 passengers
who experience
loads with the
back normal to
loads (most
optimized
configuration).
The Pods in the
2° floor on the
right and left side
have loads
perfectly in line
with the back.
All others Pods
have loads with
about 80% of the
load in line with
the back and
20% lateral.
Anti-g suits
and lateral
head stopper
on the seats
will be
enough to
counteract
an about
0.5g lateral
load.
The Passengers accomodation during flight
During the 40 min of flight the Passengers can screen on a dedicated monitor the flight data such as altitude,
speed, acceleration ratio.
In case a life risk contingency is detected the Passengers Module can be pyrotechnically cut and the Pods free
from descending independently one another, by means of embedded parachutes. This feature, unique to the
SHIPinSPACE technology could have saved the life of both the Challenger and Columbia teams.
Emergency pyrotechnic cut
Mission preparation
Passengers get trained during a 5 sessions trial spread
over a period of 2 years on machines like this centrifuge
to accomodate people the same way as they will be in
the SHIPinSPACE Vehicle.
Mission preparation
Passengers experience
the same level of
loads that will
encounter during the
flight.
Maximum
acceleration will be
2.0g during ascent
phase at the end of
the propulsion phase
and 2.5g during
maximum drag along
the descent.
Operations after landing
After landing the
Vehicle is tilted
from horizontal
to a vertical
configuration by
means of a
crane mounted
on a mobile
gantry. 2 pivot
points are fixed
on ground on
the Vehicle in
correspndence
of 2 trunnions.
Operations after landing
The vertical
configuration is
the most
appropriate to
get in/out of the
Passengers
and to spend
comfortably the
time needed for
the flight
equipment
checks,
Passengers
fastening, Pod
hatch closure
and Pod
pressurization.
Operations after landing
Operations during
the on/out board
rely on a gantry
having 3
independent floors
with a fixed part and
some mobile
plateforms that once
closed permit
accessibility
operations to be
made in parallel,
then much
optimising the time
needed to get in/out
of the Passengers
Operations before take-off
The crane will
set the Vehicle
from horizontal
to vertical in
such a way to
be located on
the launch pad
in
correspondence
of the 4 clamps
Take-off
Arms open 5 sec before take-off
On-ground clamps open only after main chamber
pressure is checked for each engine
FEM static analysis on Passenger Module
Modal analysis on Passenger Module
Transfer functions for load at Z direction
Margin of Safety for principal components
The role of CFD in the development of a new concept of space
transportation system
Lofting the wing then proofing at approach speed flight condition varying A0A, polar plot of the
configuration was drawn up
Main results: Isolated wing
Cp and polar plots for different angle of
attack from -15° to +15° were quickly
obtained for the isolated wing capable of
reaching trim condition at around 5.5°.
Wing sizes 26m in span with a lifting surface
of 232m2. AR is around 3. Wing load is
1177.2N/m2
Main Results: CRUISE GLIDING at MACH 0.3
Results in term of Coefficient of pressure was obtained
3 deg 6 deg 9 deg
12 deg
15 deg
Main Results: CRUISE GLIDING at MACH 0.3
Friction velocity path shows the evident stall at tip at 15°. This stall doesn’t
involve control surface.
15 deg
CHART: HIGHLIGHTS
Executive Summary
Phase1: Business Plan based on a $5M investment
Marketing analysis
This is the target market SiS is pursuing
Marketing analysis
 With SHIPinSPACE access to Space is not an exclusive of the
richest of the Planet anymore
 By supposing that (much conservatively) 1/1000 can have an
interest to live a Space venture we can potentially count on
7350 Passengers per year, the large difference between Offer
and Demand means an ordering book for many years to come
 Once safe Spaceships will be able to operate weekly the Space
Tourism will be considered an ordinary enjoyment Adventure
and will quickly become a “social brand” and the need to
experience it “as our friends have enjoyed”. Numbers that look
too much optimistic today will be considered normal when
many Spaceships will be operating
 It has been the same at the dawn of Aviation where the
increment of Passengers has far overcome any prediction
The business potential
 With a capacity as high as 44 Passengers, SHIPinSPACE can
open the way to a new market with 2228 Passengers yearly
 With a ticket price as low as $50k SHIPinSPACE will also lead the
market towards a Space Tourism that will much involve
Customers categories made up by passionate people wishing to
live a unique venture that also includes the 2 years of training
and preparation before the flight
 The SHIPinSPACE project opens the way to another scale of
business made up by 2288 Flight Passengers and other say 7000
persons, friends/family that will follow with the Passengers to
the Spaceport, a figure that in terms of hotel accommodation,
souvenir gifts, and other consumer deeds can much enlarge the
revenue of the Company and the surrounding local business
(bar, restaurants,…)
…Not only Flight Tickets sale
The SiS Drop Tower 55 m long
The Bluewater Mall close to London has showed
interest in accommodating the SiS Passenger Module
27 Million Visitors annually
13000 free car parking
Flight and On-Ground Sales
Sales Forecast
Year 1 Year 2 Year 3 Year 4 Year 5
Unit Sales
Flight Tickets 0 50 100 200 400
On-Ground Entertm.& Outreach (single) 0 700.000 800.000 900.000 1.000.000
On-Ground Entertm.& Outreach (family) 0 300.000 400.000 500.000 600.000
On-Ground Visitors 0 2.000.000 2.000.000 2.000.000 2.000.000
Total Unit Sales 0 3.000.050 3.200.100 3.400.200 3.600.400
Unit Prices Year 1 Year 2 Year 3 Year 4 Year 5
Flight Tickets $0 $50.000 $50.000 $50.000 $50.000
On-Ground Entertm.& Outreach (single) $0 $20 $20 $30 $30
On-Ground Entertm.& Outreach (family) $0 $50 $50 $60 $60
On-Ground Visitors $0 $5 $5 $5 $5
Sales
Flight Tickets $0 $2.500.000 $5.000.000 $10.000.000 $20.000.000
On-Ground Entertm&Outreach (single) $0 $14.000.000 $16.000.000 $27.000.000 $30.000.000
On-Ground Entertm&Outreach (family) $0 $15.000.000 $20.000.000 $30.000.000 $36.000.000
On-Ground Visitors $0 $10.000.000 $10.000.000 $10.000.000 $10.000.000
Total Sales $0 $41.500.000 $51.000.000 $77.000.000 $96.000.000
THANK YOU !

Más contenido relacionado

Similar a Boer_SHIPinSpace_Conferenza di Napoli

An Economic Analysis of the Viability of a Supersonic Business Jet
An Economic Analysis of the Viability of a Supersonic Business JetAn Economic Analysis of the Viability of a Supersonic Business Jet
An Economic Analysis of the Viability of a Supersonic Business Jet
Michael Lopez
 
High_Voltage_Design_Brief
High_Voltage_Design_BriefHigh_Voltage_Design_Brief
High_Voltage_Design_Brief
Lansing Wei
 

Similar a Boer_SHIPinSpace_Conferenza di Napoli (20)

Aviation PPT Frankfinn
Aviation PPT FrankfinnAviation PPT Frankfinn
Aviation PPT Frankfinn
 
Batangas Airport Philippines.pdf
Batangas Airport Philippines.pdfBatangas Airport Philippines.pdf
Batangas Airport Philippines.pdf
 
Aaru
AaruAaru
Aaru
 
Batangas Airport.pdf
Batangas Airport.pdfBatangas Airport.pdf
Batangas Airport.pdf
 
AVIATION PPT (RAHUL GUPTA)
AVIATION PPT (RAHUL GUPTA) AVIATION PPT (RAHUL GUPTA)
AVIATION PPT (RAHUL GUPTA)
 
Aviation (2)1
Aviation (2)1Aviation (2)1
Aviation (2)1
 
Frankfinn Aviation ppt
Frankfinn Aviation pptFrankfinn Aviation ppt
Frankfinn Aviation ppt
 
StrongMobile Flying Car Project
StrongMobile Flying Car ProjectStrongMobile Flying Car Project
StrongMobile Flying Car Project
 
Aviation ppt frankfinn
Aviation ppt frankfinn Aviation ppt frankfinn
Aviation ppt frankfinn
 
An Economic Analysis of the Viability of a Supersonic Business Jet
An Economic Analysis of the Viability of a Supersonic Business JetAn Economic Analysis of the Viability of a Supersonic Business Jet
An Economic Analysis of the Viability of a Supersonic Business Jet
 
SRM- JSM - AIRPORTS-30 0CT 13.pptx
SRM- JSM - AIRPORTS-30 0CT 13.pptxSRM- JSM - AIRPORTS-30 0CT 13.pptx
SRM- JSM - AIRPORTS-30 0CT 13.pptx
 
Frankfinn - Aviation
Frankfinn - AviationFrankfinn - Aviation
Frankfinn - Aviation
 
Airbus
AirbusAirbus
Airbus
 
High_Voltage_Design_Brief
High_Voltage_Design_BriefHigh_Voltage_Design_Brief
High_Voltage_Design_Brief
 
Airport apron and holding bays
Airport apron and holding baysAirport apron and holding bays
Airport apron and holding bays
 
Airport terminal planning and design
Airport terminal planning and designAirport terminal planning and design
Airport terminal planning and design
 
Senior Design Project report
Senior Design Project reportSenior Design Project report
Senior Design Project report
 
Presentation airport planning
Presentation airport planningPresentation airport planning
Presentation airport planning
 
K@ran sa hu
K@ran sa huK@ran sa hu
K@ran sa hu
 
UNIT-3.pptx
UNIT-3.pptxUNIT-3.pptx
UNIT-3.pptx
 

Boer_SHIPinSpace_Conferenza di Napoli

  • 1. 44 PASSENGERS + 4 P/L’s SUB-ORBITAL REUSABLE BLASTING SURVIVAL VEHICLE 22 October 2014 – Naples Conference: «How to create jobs with the new Aerospace Industry»
  • 2. S/S Equipment bay Light weight shock-absorber Fairing made up by Carbon Fibre (CFRP) sandwich panels
  • 3. Pod Equipment bay (parachutes, batteries, tanks,...) Light weight shock-absorber Cone pyro-separation detail Panel for S/S Equipment in the most protected area
  • 4. The Pod •Typical accomodation of 4 Passengers •It is the only pressurized part of the SHIPINSPACE vehicle •Seat design tailored to extra large people having seats width of 650 mm against the 450 typical of an economic class. •Seats are designed in such a way Passengers can withstand lateral loads (0,5g) •Seats packaging can rotate along the axis normal to the window S/S’s volume (unpressurized)
  • 5. The Pod The internal configuration (shown in this artistic view) will have COSMO-like internal wall painting with small led providing a unique suggestion scenario. Passengers will have the impression to be in a continuous media with the outside view. Mission screen with major parameters will be embedded in a seat packaging arm.
  • 6. View of the Passengers close to the window The 800 mm diameter window, 7 times larger than a wide-body Aircraft one, will permit an outstanding view of outside even for the 2 Passengers close to the window. During the 6 min of 0-g the Passengers can move freely inside the Module getting their preferred outside picture
  • 7. View of the Passengers located far from the hatch port During the 6 min of 0-g at the top of the Parabolic flight Passengers experience weightlessness in free flying inside the Pod. An ergonomic study could verify that the space around the Passengers is higher than that of a business class of a wide-body aircraft
  • 8. Mission details Slight rotation along Z axis to let Passengers having the same view Manoeuvering phase Landing phase
  • 9. Passengers configuration during descent and landing The loads during the descent are normal to this figure plane. The Pods in the 2° floor and in the middle have only 2 passengers who experience loads with the back normal to loads (most optimized configuration). The Pods in the 2° floor on the right and left side have loads perfectly in line with the back. All others Pods have loads with about 80% of the load in line with the back and 20% lateral. Anti-g suits and lateral head stopper on the seats will be enough to counteract an about 0.5g lateral load.
  • 10. The Passengers accomodation during flight During the 40 min of flight the Passengers can screen on a dedicated monitor the flight data such as altitude, speed, acceleration ratio. In case a life risk contingency is detected the Passengers Module can be pyrotechnically cut and the Pods free from descending independently one another, by means of embedded parachutes. This feature, unique to the SHIPinSPACE technology could have saved the life of both the Challenger and Columbia teams. Emergency pyrotechnic cut
  • 11. Mission preparation Passengers get trained during a 5 sessions trial spread over a period of 2 years on machines like this centrifuge to accomodate people the same way as they will be in the SHIPinSPACE Vehicle.
  • 12. Mission preparation Passengers experience the same level of loads that will encounter during the flight. Maximum acceleration will be 2.0g during ascent phase at the end of the propulsion phase and 2.5g during maximum drag along the descent.
  • 13. Operations after landing After landing the Vehicle is tilted from horizontal to a vertical configuration by means of a crane mounted on a mobile gantry. 2 pivot points are fixed on ground on the Vehicle in correspndence of 2 trunnions.
  • 14. Operations after landing The vertical configuration is the most appropriate to get in/out of the Passengers and to spend comfortably the time needed for the flight equipment checks, Passengers fastening, Pod hatch closure and Pod pressurization.
  • 15. Operations after landing Operations during the on/out board rely on a gantry having 3 independent floors with a fixed part and some mobile plateforms that once closed permit accessibility operations to be made in parallel, then much optimising the time needed to get in/out of the Passengers
  • 16. Operations before take-off The crane will set the Vehicle from horizontal to vertical in such a way to be located on the launch pad in correspondence of the 4 clamps
  • 17. Take-off Arms open 5 sec before take-off On-ground clamps open only after main chamber pressure is checked for each engine
  • 18. FEM static analysis on Passenger Module
  • 19. Modal analysis on Passenger Module
  • 20. Transfer functions for load at Z direction
  • 21. Margin of Safety for principal components
  • 22. The role of CFD in the development of a new concept of space transportation system
  • 23. Lofting the wing then proofing at approach speed flight condition varying A0A, polar plot of the configuration was drawn up Main results: Isolated wing Cp and polar plots for different angle of attack from -15° to +15° were quickly obtained for the isolated wing capable of reaching trim condition at around 5.5°. Wing sizes 26m in span with a lifting surface of 232m2. AR is around 3. Wing load is 1177.2N/m2
  • 24. Main Results: CRUISE GLIDING at MACH 0.3 Results in term of Coefficient of pressure was obtained 3 deg 6 deg 9 deg 12 deg 15 deg
  • 25. Main Results: CRUISE GLIDING at MACH 0.3 Friction velocity path shows the evident stall at tip at 15°. This stall doesn’t involve control surface. 15 deg
  • 26. CHART: HIGHLIGHTS Executive Summary Phase1: Business Plan based on a $5M investment
  • 27. Marketing analysis This is the target market SiS is pursuing
  • 28. Marketing analysis  With SHIPinSPACE access to Space is not an exclusive of the richest of the Planet anymore  By supposing that (much conservatively) 1/1000 can have an interest to live a Space venture we can potentially count on 7350 Passengers per year, the large difference between Offer and Demand means an ordering book for many years to come  Once safe Spaceships will be able to operate weekly the Space Tourism will be considered an ordinary enjoyment Adventure and will quickly become a “social brand” and the need to experience it “as our friends have enjoyed”. Numbers that look too much optimistic today will be considered normal when many Spaceships will be operating  It has been the same at the dawn of Aviation where the increment of Passengers has far overcome any prediction
  • 29. The business potential  With a capacity as high as 44 Passengers, SHIPinSPACE can open the way to a new market with 2228 Passengers yearly  With a ticket price as low as $50k SHIPinSPACE will also lead the market towards a Space Tourism that will much involve Customers categories made up by passionate people wishing to live a unique venture that also includes the 2 years of training and preparation before the flight  The SHIPinSPACE project opens the way to another scale of business made up by 2288 Flight Passengers and other say 7000 persons, friends/family that will follow with the Passengers to the Spaceport, a figure that in terms of hotel accommodation, souvenir gifts, and other consumer deeds can much enlarge the revenue of the Company and the surrounding local business (bar, restaurants,…)
  • 30. …Not only Flight Tickets sale The SiS Drop Tower 55 m long
  • 31. The Bluewater Mall close to London has showed interest in accommodating the SiS Passenger Module 27 Million Visitors annually 13000 free car parking
  • 32. Flight and On-Ground Sales Sales Forecast Year 1 Year 2 Year 3 Year 4 Year 5 Unit Sales Flight Tickets 0 50 100 200 400 On-Ground Entertm.& Outreach (single) 0 700.000 800.000 900.000 1.000.000 On-Ground Entertm.& Outreach (family) 0 300.000 400.000 500.000 600.000 On-Ground Visitors 0 2.000.000 2.000.000 2.000.000 2.000.000 Total Unit Sales 0 3.000.050 3.200.100 3.400.200 3.600.400 Unit Prices Year 1 Year 2 Year 3 Year 4 Year 5 Flight Tickets $0 $50.000 $50.000 $50.000 $50.000 On-Ground Entertm.& Outreach (single) $0 $20 $20 $30 $30 On-Ground Entertm.& Outreach (family) $0 $50 $50 $60 $60 On-Ground Visitors $0 $5 $5 $5 $5 Sales Flight Tickets $0 $2.500.000 $5.000.000 $10.000.000 $20.000.000 On-Ground Entertm&Outreach (single) $0 $14.000.000 $16.000.000 $27.000.000 $30.000.000 On-Ground Entertm&Outreach (family) $0 $15.000.000 $20.000.000 $30.000.000 $36.000.000 On-Ground Visitors $0 $10.000.000 $10.000.000 $10.000.000 $10.000.000 Total Sales $0 $41.500.000 $51.000.000 $77.000.000 $96.000.000