Johnson Space Center Aircraft Operations Division Overview

1
N95NA
Baseline Science Modifications
Gulfstream V
Gulfstream V
Serial 672, built in 2002
Service Ceiling: 51,000ft
Max Gross Weight: 90,900lbs
Max Mission Duration: 12hrs
Max Cabin Payload: 8,100lbs
Max Speed: Mach 0.885
Normal cruise range: >5,000nm
2
Portals
Two downward-facing portals installed in forward cabin
3
Portals
Two downward-facing portals installed in forward cabin
20.75” x 20.75” opening in each portal adapter
Instruments installed either suspended from the floor above or bolted directly to the portal adapter
350lb can be mounted directly to each ring frame adapter
JSC-designed window pack can also be mounted in the ring frame adapter
Can accommodate up to a 17.4 DIA window
Shutter will be available for debris impact protection
4
Windows
Window Adapter Baseline Design
17.4” viewable window pack
Single pane, ~1.5” thick
Recessed for debris protection
Design flexible to incorporate other windows, e.g.
DC-8 windows
5
Aircraft Frame
Window Adapter
Window Pack
Retainer
O-ring seal
Gasket seal
Window Pack
Expanded Section
View
Aluminum
Frame
Glass Pane
(various materials)
Silicone Rubber
Gasket X2
Silicone Rubber
Bumper
Cabin Layout
Power and Control Rack – houses all network, computer equipment, and power equipment for payload support
Mission Specific Payload Area
Up to 8 equipment rack/seat locations in cabin
Full restraint seats available to monitor equipment during takeoff and landing
Standard number of passengers: 5
More possible if seats installed in payload area: mission dependent
Cabin Layout
6
Power and Control Racks
Mission-Specific Payload Area
RF/Data/Power Distribution
Network/RF Connection Overlay
10GBASE-T over S/FTP Cat 6A
OM1 and OM3 fiber rack-to-rack connectivity
SF-142 coax to each rack position for GPS/RF signals
Configurable via patch panel on control rack
Two GPS antennas installed on aircraft dedicated for payloads
Overhead conduit available between rack positions
Overall max load: 40kVA
21 kVA, 115 VAC 60 Hz (single phase)
20 kVA, 115 VAC 400 Hz (both single and three-phase)
10kW, 28 VDC (regulated)
NEMA, SAE AS6129, or NASA Mk I/III EIP power interfaces available
7
SATCOM Provisions
Iridium
5 dual-element Iridium Antennas installed
5/10 elements used
1 ASP-Provided handset (voice + data)
Iridium Extreme 9575
4-channel modem on NASDAT
9600bps max
Bandpass Filtering on all Iridium connections
Inmarsat
High Gain Antenna capable of 432kbps
Software upgradeable to 650 kbps HDR service
8
Equipment Racks
Equipment Racks
22”W x 25”D x 51”H
Biggest racks that can fit in GV while maintaining aisle width
25U available space (1U = 1.75”)
Maximum weight: 340lbs
Empty weight: ~50lbs
Maximum overturning moment: 6225 in-lbs
9
Equipment Racks
Costs, Mission
Science customers only charged variable cost per flight hour
(gas, spares, engine maintenance) 
plus
 MPCs
$3K per flight hour, FY19
MPCs include per diem, lodging, rental cars, air fare, FBO
costs, fuel surcharges, mechanic overtime, and some
management reserve
Aircraft deploys with two pilots, two mechanics, and one
FSO on most missions
»
Would double crew to provide OIB-like missions
capacity to fly multiple days in a row at maximum
range/endurance
10
Equipment Racks
Contact Information
Program Manager
Derek Rutovic, 832-205-3854
Project Engineers
Charlie Marshik, 281-796-2473
Tyler Thompson, 832-692-6850
Project Pilots
Bill Rieke, 281-799-5463
Ken Cook, 281-244-0971
11
Slide Note
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Johnson Space Center's Aircraft Operations Division features the Gulfstream V aircraft with unique modifications like downward-facing portals, specialized windows, and mission-specific payload support areas. The aircraft is designed for high-altitude operations with a service ceiling of 51,000 feet and a maximum speed of Mach 0.885. It includes advanced features such as power and control racks, seating for up to 5 passengers, and the capability to accommodate various mission payloads.

  • Johnson Space Center
  • Aircraft Operations
  • Gulfstream V
  • High-altitude Operations
  • Mission Payload

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  1. Aircraft Operations Division Johnson Space Center N95NA Baseline Science Modifications 1

  2. Aircraft Operations Division Johnson Space Center Gulfstream V Gulfstream V Serial 672, built in 2002 Service Ceiling: 51,000ft Max Gross Weight: 90,900lbs Max Mission Duration: 12hrs Max Cabin Payload: 8,100lbs Max Speed: Mach 0.885 Normal cruise range: >5,000nm 2

  3. Aircraft Operations Division Johnson Space Center Portals Two downward-facing portals installed in forward cabin 24.07 24.20 3

  4. Aircraft Operations Division Johnson Space Center Portals Two downward-facing portals installed in forward cabin 20.75 x 20.75 opening in each portal adapter Instruments installed either suspended from the floor above or bolted directly to the portal adapter 350lb can be mounted directly to each ring frame adapter JSC-designed window pack can also be mounted in the ring frame adapter Can accommodate up to a 17.4 DIA window Shutter will be available for debris impact protection 4

  5. Aircraft Operations Division Johnson Space Center Windows Window Adapter Baseline Design 17.4 viewable window pack Single pane, ~1.5 thick Recessed for debris protection Design flexible to incorporate other windows, e.g. DC-8 windows Retainer Window Pack O-ring seal Aluminum Frame Glass Pane (various materials) Window Adapter Gasket seal Silicone Rubber Bumper Window Pack Expanded Section View Aircraft Frame Silicone Rubber Gasket X2 5

  6. Aircraft Operations Division Johnson Space Center Cabin Layout Cabin Layout Power and Control Rack houses all network, computer equipment, and power equipment for payload support Mission Specific Payload Area Up to 8 equipment rack/seat locations in cabin Full restraint seats available to monitor equipment during takeoff and landing Standard number of passengers: 5 More possible if seats installed in payload area: mission dependent Mission-Specific Payload Area Power and Control Racks 6

  7. Aircraft Operations Division Johnson Space Center RF/Data/Power Distribution Network/RF Connection Overlay 10GBASE-T over S/FTP Cat 6A OM1 and OM3 fiber rack-to-rack connectivity SF-142 coax to each rack position for GPS/RF signals Configurable via patch panel on control rack Two GPS antennas installed on aircraft dedicated for payloads Overhead conduit available between rack positions Overall max load: 40kVA 21 kVA, 115 VAC 60 Hz (single phase) 20 kVA, 115 VAC 400 Hz (both single and three-phase) 10kW, 28 VDC (regulated) NEMA, SAE AS6129, or NASA Mk I/III EIP power interfaces available 7

  8. Aircraft Operations Division Johnson Space Center SATCOM Provisions Iridium 5 dual-element Iridium Antennas installed 5/10 elements used 1 ASP-Provided handset (voice + data) Iridium Extreme 9575 4-channel modem on NASDAT 9600bps max Bandpass Filtering on all Iridium connections Inmarsat High Gain Antenna capable of 432kbps Software upgradeable to 650 kbps HDR service 8

  9. Aircraft Operations Division Johnson Space Center Equipment Racks Equipment Racks 22 W x 25 D x 51 H Biggest racks that can fit in GV while maintaining aisle width 25U available space (1U = 1.75 ) Maximum weight: 340lbs Empty weight: ~50lbs Maximum overturning moment: 6225 in-lbs 9

  10. Aircraft Operations Division Johnson Space Center Equipment Racks Costs, Mission Science customers only charged variable cost per flight hour (gas, spares, engine maintenance) plus MPCs $3K per flight hour, FY19 MPCs include per diem, lodging, rental cars, air fare, FBO costs, fuel surcharges, mechanic overtime, and some management reserve Aircraft deploys with two pilots, two mechanics, and one FSO on most missions Would double crew to provide OIB-like missions capacity to fly multiple days in a row at maximum range/endurance 10

  11. Aircraft Operations Division Johnson Space Center Equipment Racks Contact Information Program Manager Derek Rutovic, 832-205-3854 Project Engineers Charlie Marshik, 281-796-2473 Tyler Thompson, 832-692-6850 Project Pilots Bill Rieke, 281-799-5463 Ken Cook, 281-244-0971 11

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