1. PROJECT PROPOSAL

2. Agenda
Micro Satellite Market Overview
System Description
Performance
Project Estimates
Implementation Timeline
Summary

3. Microsat Market: Capacity
SpaceWorks forecast:
Micro Sat ( kg)
Nano Sat (1-10 kg)
Project goal: 30% market share by 2020 (20-25 launches per year)

4. Applications & Users Microsat Constellations:
SpaceWorks forecast:
Microsat Constellations:
Earth Observation:
BlackSky Global (44 kg) – 60
Hera (24 kg) – 48
Iceye (<100 kg) – 50
OmniEarth (110 kg) – 15
PlanetLabs (5-150 kg) – 100
Satellogic (35 kg) – 300
TerraBella (120 kg) – 24
Earth Science
GeoOptics (100 kg) – 24
PlanetiQ (20 kg) – 22
Telecommunication
ORBCOMM ( kg) – 47
OneWeb ( kg) – 648
SpaceX ( kg) – 4000

5. Key Customers & Their Needs
Universities & educational institutions
space experiments from idea to results within 1 year
simple payload integration
Innovation & startups
quick spacecraft deploy
possibility for nonstandard orbit insertion
technology leaking risk reduction
Business & government
solutions in case of emergencies
urgent delivery into orbit

6. Current Capabilities Piggyback Launch: ESPA, ASAP & SHERPA
Cluster Launch
Dedicated Launch
Pro:
standard spacecraft integration procedure
shorter time to launch
Cons:
safety restrictions (rocket motors, high pressure vessels etc.)
orbit limited by primary payload
Pro:
non-standard spacecraft can be launched
individually tuned orbit
Cons:
long wait before launch (up to 2 yrs)
spacecraft integration can be complicated
Pro:
any spacecraft
any orbit
Cons:
expensive due to
existing launch vehicles

7. Solution
Provide a fast, reliable & efficient access to Earth orbit by offering launch services close to a customer with a flexible aerospace system worldwide
innovative solution for micro/nano spacecrafts
relative low launch cost per payload weight
spacecraft integration and launch next to a client worldwide
instant mission implementation
any orbit, any application

8. LV Onboard the Carrier LV liftoff mass, ton 15 Launch point range, km
Launch Equipment
LV liftoff mass, ton 15
Launch point range, km
1000
Airdrop altitude, m
9000
Airdrop velocity, km/h
650

9. LV Onboard the Carrier LV liftoff mass, ton 15 Launch point range, km
Airdrop Platform
Launch Equipment
Launch Vehicle
Eject chute
Il-76 plane
LV liftoff mass, ton 15
Launch point range, km
1000
Airdrop altitude, m
9000
Airdrop velocity, km/h
650

10. LV Design Launch weight, ton 13.9 Case diameter/overall length, m
Fairing
Payload
Avionics bay
3rd stage motor &RCS
2nd stage motor &RCS
Fins (4)
Interstage bay & FTS
1st stage motor
Launch weight, ton
13.9
Case diameter/overall length, m
1.1/14.6
Spacecraft weight: SSO(700 km, 98.8°)/ LEO(220 км, 45°), kg
100/200
Payload bay size, m
Ø1.0х1.6
Boost overloads, g
10…15
Wings (4)
Fin servos & 1st stage RCS

11. System Concept Solid Propellant Launch Vehicle Air Launch Plane
Homeland
LV Assembly, Test & Prepare Facility
Mobile Inflatable
Spacecraft Mount Facility

12. Operation Scheme Fly to Customer Airfield – Worldwide
LV assembly,
Test & ALC Load
Fly to Customer Airfield – Worldwide
SC Mount Facility Deploy
LV Integration
Fly to Launch Point & LV Airdrop

13. Launch Scheme Stage 3 Burnout, SC Release: H=700 km, V=7510 m/s
Stage 1 Separation, Fairing Jettison,
Stage 2 SRM Ignition:
H=116 km
V=2945 m/s
t=123.0 s
Θ=23°
Stage 2 Separation, Stage 3 SRM Ignition:
H=700 km
V=4943 m/s
t=628.0 s
Θ=0.67°
Airdrop:
H=9 km
V=180 m/s
t=0.0 s
Θ=0°
Pull-up:
H=8.35 km
V=404 m/s
t=16.0 s
Θ=0°
ny=2.5 g
Max Q:
H=11.5 km
V=686 m/s
t=32.0 s
Θ=32° M=3.0
Platform Separation:
H=8.97 km
V=165 m/s
t=3.4 s
Θ=-17°
Stage 1 SRM Ignition:
H=8.90 km
V=170 m/s
t=5.0 s
Θ=-23°

14. Carrier Craft Features
Launch point range, km
2,000
Airdrop altitude, m
9,000
Airdrop velocity, km/h
650

15. Energetic Data

16. Competitive Advantages
Piggyback & cluster launch opportunities:
SpaceX, ULA, ESA, Roskosmos, ISRO etc.
long launch preparation time
spacecraft restrictions
limited orbits
currently in use
Dedicated Ground Launch Vehicles:
Electron, Vector-H, SS-520-4, SMILE
spacecraft delivered to a launch site
maiden launch in
ground test passed in 2016
Airdrop LV
ready for launch worldwide
quick insertion into orbit
instant mission preparation
maiden launch in 2020
Ukraine
China

17. AiLEO Launch Cost

18. Total project development cost $135M
Project Estimates
Parameter
Pegasus XL
Electron
UA ALV
Launches per year
1 (2016)
120 (max.)
12 (est.)
Liftoff weight, т
23.13
10.5
13.9
Diameter/length, m
1.27 / 16.94
1.2 / 17.0
1.1 / 14.5
Payload SSO(700x98.2°)/LEO (220x45°), kg
220 / 420
120 / 225
100 / 220
Payload bay size, m
Ø1.15х2.14
Ø1.0х1.6
Ø0.9х1.6
User launch price, M$
55.0
4.9
3.4
Cost per kilogram on LEO, M$/k$
130.9
21.7
15.5
ROI, launches/years
68 / 5.7
Total project development cost $135M

19. Airdrop Project Production
System
Poland
Ukraine
Launch Vehicle assembly, test & prelaunch operations
Solid rocket motors
Fin servos
Avionics
H2O2 Reaction Control System
Fairing
Carrier plane, launch equipment & navigation
Airdrop platform
Descent chute & control system
Ground support equipment

20. Implementation Timeline
Year 1
Year 2
Year 3 I II
III IV
Phase 2a. Development
Phase 2b. Development & tests
Avionics
Launch vehicle
Ground support equipment
Carrier plane
Airdrop platform
Phase 3. Production & tests
Maiden launch

21. Thank you for attention!
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