1. Your resources
provided by ISS
Your view
to the stars
Your payload
hosting slot
Bartolomeo –
Commercial External Payload Hosting Facility On ISS
Your view
to Earth
Remote
Sensing
Astrophysics
Heliophysics
Atmospheric
Research
Space Weather
On-orbit
Assembly for
Exploration
Robotics
Testing
In-orbit Testing
Space Science
Spacecraft
Deployment
In-space
Manufacturing

2. ISS FWD
ISS Zenith
Bartolomeo –
Commercial External Payload Hosting Facility On ISS
● Perfect view to Earth and the stars
● Unpressurized payload accommodation with power, data and active cooling
● Instrument stabilization and pointing with Teledyne Brown MUSES
● Various payload sizes up to FRAM standard available
● Pressurized and unpressurized launch options
● Mission service available in 2018
ISS Nadir
JCAP-based
payloads compliant
with JEM-A/L
envelopeFRAM-based
payloads
FRAM Extension Kit
Teledyne Brown
MUSES
Active Cooling
System
European
Columbus
Module
View Obscuration Zenith Nadir Ram Wake
Minimum 22.4% 1.1% 0% 44.6%
Maximum 34.4% 8.7% 5.3% 47.0%
WakeForwardNadirZenith

3. Payload Type JCAP-based Payloads FRAM Standard Payloads
Quantity of sites 6 6
Field of view • All Nadir and Zenith view
• 4 slots Ram view
• 2 slots Zenith and Ram view
• 2 slots Nadir, Ram, Wake
• 1 slot Zenith, Ram,
Starboard
• 1 slot Nadir, Ram,
Starboard
Geometric envelopes 640 x 830 x 1000 mm1 864 x 1168 x 1245 mm 864 x 1168 x 1245 mm
Mass per payload up to 100 kg nominal2 up to 599 kg nominal2,3 up to 300 kg nominal2,3
Power per payload • 2 x 28 Vdc operational power
up to
50 W per each slot
• 1 x 28 Vdc 100 W additional
power selectable for one slot
at a time
• 120 Vdc operational power
up to 800 W, CEPA
compatible4
• 120 Vdc operational power,
ExPA compatible5
• 120 Vdc operational
power, ExPA compatible5
Data rate to ISS up to 100 Mbit/s via Bartolomeo
wireless system
up to 100 Mbit/s via Bartolomeo
wireless system
up to 100 Mbit/s via
Bartolomeo wireless system
Cooling capability - • 1 Nadir site, 1 Zenith site
• Up to 1.5 kW total cooling
capability
-
Robotic interface SPDM micro fixture SPDM micro fixture SPDM micro fixture
Return capability Yes, if JEM-A/L compatible No No
Payload to platform
interface
JCAP bracket and electrical
connector
P-FRAM standard, P-FRAM
modified with fluid interface
P-FRAM standard
1 Geometric envelope constrained by JEM-A/L dimensions, envelope
can be extended if payload is launched unpressurized.
2 Overall payload mass budget of the platform is 2800 kg.
3 FRAM capability depends on payload center of gravity position
4 Power routed from European Columbus Module.
5 Power routed from ISS US Orbital Segment.
Payload transfer to outside
Payload robotic
installation
Payload mission
Payload launch
Mission Duration 1 – 7 yearsMission Lead Time 1 – 1.5 years
Payload data
processing
and delivery
Standard Payload Sizes & Resources
All-in-one Mission
Service
● All mission elements in
one service contract
● Reliable integrated
mission solution

4. Airbus Defence and Space
Space Systems
Airbus DS GmbH
On-orbit Services and Exploration
Airbus-Allee 1, 28199 Bremen, Germany
Dr. Christian Steimle, Project Manager
per-christian.steimle@airbus.com
https://de.linkedin.com/in/dr-per-christian-
steimle-46217b8a
Airbus DS Space Systems Inc.
555 Forge River Road, Suite 115
Webster, TX 77598, United States of America
Ron Dunklee, President and CEO
rdunklee@airbusdshouston.com
https://www.linkedin.com/in/rondunklee
www.airbusdefenceandspace.com
Airbus DS GmbH
On-orbit Services and Exploration
Airbus-Allee 1, 28199 Bremen, Germany
Carlo Mirra, Director Space Products Sales
carlo.mirra@airbus.com
https://de.linkedin.com/in/carlo-mirra-97124517