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Naval Postgraduate School 2009 CubeSat Developers Workshop California Polytechnic State University Naval Postgraduate School Space Systems Academic Group Monterey, CA 93943 NPS CubeSat Launcher (NPSCuL) Program Update LCDR Adam “Tito” DeJesus, USN (I&T Manager) LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG Anthony Harris (Sequencer System Design) Dr. Jim Newman ( Professor, Space Systems)

NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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Page 1: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

Naval Postgraduate School2009 CubeSat Developers WorkshopCalifornia Polytechnic State University

Naval Postgraduate SchoolSpace Systems Academic Group

Monterey, CA 93943

NPS CubeSat Launcher (NPSCuL) Program Update

LCDR Adam “Tito” DeJesus, USN (I&T Manager)

LT Christina Hicks, USN (Program Manager)LT Matthew Crook, USN (Structural Design)

LTJG Anthony Harris (Sequencer System Design)Dr. Jim Newman ( Professor, Space Systems)

Page 2: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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What is “coach class” on a rocket?

Page 3: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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What is “coach class” on a rocket?

The “airliners” of the US unmanned space program.

DELTA ATLAS

Page 4: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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Seating Arrangement

First Class

Business Class

What is “coach class” on a rocket?

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The under-served customer

And

The “limited leg-room” seat

What is “coach class” on a rocket?

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What is “coach class” on a rocket?

Seating Arrangement

First Class

Business Class

Coach Class?

Page 7: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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P-PODs packaged as a secondary payload.

-high capacity (24U-50U)

-leverages mature technology

-multi-LV compatible

-low risk to primary payload or other secondary payloads

This is the Coach Class Section!

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NPSCuL Design

Figure 1 – NPSCuL Standard (Left) and NPSCuL Lite (Right)NPSCuL (10 5U P-PODS)

(ESPA-Compatible)

NPSCuL-Lite (8 3U P-PODS)

(Compatible with ESPA and other, smaller Secondary

Payload Adapters)

Page 9: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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Integration Process

DoD / Government/ University CubeSat Experiments

Launch!

Space Test Program

(or other launch provider)

P-PODS integrated into NPSCuL structure

Finished NPSCuL delivered to Space Vehicle Integration Site

Integrated P-PODs

CubeSats integrated into P-PODSFinished P-PODs delivered to NPSCuL Integration Site Space Vehicle Integration

and flight preparation

Page 10: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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NPSCuL-LITE Test Program

Structure Qualification– Launch environments +6dB using Mass Models to

simulate loaded P-PODs– Must accommodate minimum expected CubeSat

mass (1 kg/U)– NPS will perform all structural tests

Functional Developmental Testing– On-board electronics fire the deployment

systems in sequence– Currently in development by a launch provider– NPS to develop mission specific electrical

harnesses

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Sequencer Design

Requirements:

•28V power from LV

•RS-422 programming interface

•8-channel redundant output

Page 12: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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Program Progress To Date

NPSCuL-Lite– Qualification Test structure

produced and assembled.– Mass model of sequencer unit has

been integrated – Structural and TVAC testing to

begin shortly.P-POD Mass Models

– 9 units produced– design went through a thorough

qualification test batterySequencer – development by industry is

underway.

Page 13: NPS Cubesat Launchermstl.atl.calpoly.edu/~workshop/archive/2009/Spring... · 2016. 3. 16. · LT Christina Hicks, USN (Program Manager) LT Matthew Crook, USN (Structural Design) LTJG

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Program Progress To Date

P-POD Mass Model Structural Test at NPS Vibration Test Facility, Monterey, CA

20 100 1000 2000

[Hz]

0.01

0.1

1

[g]

X: 850[Hz]Y: 4.47[g]

Chan.no: 2Chan.type: M FilteredSweep type: logarithmicSweeps done: 1Sweeps req.: 2Sweep direct.: upSweep rate: 4.00 Oct/minContr.strat.: AverageUnit: gContr.strat.: Closed loop

-- Testing time --elapsed: 000:01:39remaining: 000:01:39

Date: 04-01-09Time: 10:31:11

P2M2_at_CGSine

20 100 1000 2000

[Hz]

0.01

0.1

1

[g]

X: 850[Hz]Y: 4.47[g]

Chan.no: 2Chan.type: M FilteredSweep type: logarithmicSweeps done: 1Sweeps req.: 2Sweep direct.: upSweep rate: 4.00 Oct/minContr.strat.: AverageUnit: gContr.strat.: Closed loop

-- Testing time --elapsed: 000:01:39remaining: 000:01:39

Date: 04-01-09Time: 10:31:11

P2M2_at_CGSine

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Future of NPSCuL/NPSCuL-Lite

Potential flight opportunity exists in 2010. To support this opportunity:– Flight Article Build – through DEC 2009– Harness Design and Build – through JAN 2010– Acceptance Test– no later than March 2010

• Requires sequencer and 8 integrated, flight-ready P-PODs– Launch Vehicle Integration – April 2010– 1st Launch – August 2010

2nd Flight Opportunity – Possible slot on an ESPA ring expected in 2012– NPS will seek to fill any unfilled slots with payloads from

University developers

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Coach Class to OrbitNPSCuL

Questions?

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NPSCuL Contacts

• Principal Investigators:Dr. Jim NewmanProfessor, Space Systems Academic Group, NPS(831) [email protected]

Dr. Rudy PanholzerChairman, SSAG, NPS(831) [email protected]

Mr. Dan Sakoda Research Associate, SSAG, [email protected]

• Project Manager:LT Christina [email protected]