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ASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary level of information as described in Company Procedure J103 (or remove) Since 1958 Astro Aerospace has helped enable complex missions to Earth orbit, Mars, and beyond with innovative deployable structures and mechanisms AstroMesh® Mesh Antenna Reflector Storable Tubular Extendable Member (STEM™) Telescopic Booms Hinges and Mechanisms Hundreds of flights – Zero Failures Voyager Mars Pathfinder ISS Mobile Transporter Inmarsat 4 Alphasat 2014 Launch Pending: Soil Moisture Active Passive (SMAP) Click Here for Overview Video Cleared for public release; NGAS Case 14-1846 dated 9/10/14

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Page 1: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

Astro Aerospace

1

Use this space to communicate your key takeaway (or remove)

Mark pages according to the proprietary level of information as described in Company Procedure J103 (or remove)

Since 1958 Astro Aerospace has helped enable complex missions to Earth orbit, Mars, and beyond with innovative deployable structures and mechanisms

– AstroMesh® Mesh Antenna Reflector – Storable Tubular Extendable Member (STEM™) – Telescopic Booms – Hinges and Mechanisms

Hundreds of flights – Zero Failures – Voyager – Mars Pathfinder – ISS Mobile Transporter – Inmarsat 4 – Alphasat – 2014 Launch Pending: Soil Moisture Active Passive

(SMAP)

Click Here for Overview Video

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 2: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

AstroMesh™ Reflectors

2

http://www.northropgrumman.com/BusinessVentures/AstroAerospace/Products/Pages/AstroMesh.aspx

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 3: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

• Proven: 8 AstroMesh™ reflectors successfully deployed on-orbit

• Inherently Reliable Robust Deployment Kinematics

• Accurate Surface Repeatability

• Efficient Drum-Like Structure

• High Deployed Stiffness

• Exceptionally Low mass

• High Thermal Stability

• Easily Scales

• ESD Compatible Design & PIM Free

• High structural stiffness & RF test in 1g environment at all frequencies

AstroMesh Advantage

Most Reliable Reflector Technology Available 3

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 4: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

THURAYA/GEM 12-m AstroMesh L-Band

Deployed D1 - 11/2000 D2 - 7/2003 D3 -1/2008

Proven On-Orbit Performance

• AstroMesh has been steadily developed as a product since 1990 • 8 units deployed on-orbit and are performing flawlessly

• 2 additional deployments scheduled for 2014 • 100% On-Orbit Success – No Failures – No Anomalies

AstroMesh Reflector Flight Heritage

4

MBSat 12-m AM-1 S-Band

Deployed 3/2004

INMARSAT 4 9-m AM-1 L-Band Deployed FM1 - 3/2005 FM2 - 11/2005 FM3 - 8/2008

Alphasat 11-m AM-1 L-Band

Deployed 8/2013

Classified

Deployed Pending

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 5: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

Evolution of AstroMesh Family

5

AM-2 18 to 50-Meter

Class

Thuraya

AM 12-Meter

INMARSAT, MBSat & Alphasat

AM-1 6 to 25-Meter Class

AM-Lite 3 to 8-Meter

Class

Reduce Stowed Diameter by 40%

Reduce Reflector Mass by 50%

• AstroMesh hardware designs for a broad spectrum of applications

– Aperture sizes from 3 to greater than 50-meter – Frequency range UHF to beyond Ka-Band

Reduce Stowed Height by 40%

SMAP

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 6: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

Comparison of Stowed Packages (12-Meter Aperture)

6

3.81

AM

THURAYA

AM-1 AM-2

Starshade

2.49

3.86

The first flight design

Tighter stowed package to enable mounting on

Spacecraft sidewall

Redesigned truss articulation reduces

stowed height

INMARSAT, MBSat & Alphasat

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 7: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

AM-1 configuration

• Reduced Diameter versus 1st Generation AM – Stowed Diameter 60% of AM – Stows on Spacecraft Sidewall

• Scalable From 6 to 25-meter Aperture • Extensive Flight Heritage

– 9-m Aperture Inmarsat 4 – 12-m Aperture MBSat – 11-m Aperture Alphasat

AM 12-Meter

AM-1 6 to 25-Meter

Class

Reduce Stowed Diameter by 40%

Thuraya Inmarsat & MBSat

MBSat Inmarsat 4 Alphasat 7

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 8: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

AM-1 & AM-Lite Deployment Sequence

8

Stowed Release & Bloom Motorized Deployment

Fully Deployed & Latched

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 9: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

AM-2 Configuration

AM-2 18 to 50-

Meter Class

AM-1 6 to 25-Meter

Class

Reduce Stowed Height by 40%

• AM-2 Stows into Batten Length • AM-1 Stows in Batten Plus Longeron Lengths

• AM-2 Deployed Truss Configuration Identical to AM-1

NASA Star Occulter Development Model

9 Cleared for public release; NGAS Case 14-1846 dated 9/10/14

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ASTRO AEROSPACE

AM-2 Deployment Sequence

Stowed Release & Bloom Motorized Deployment

Fully Deployed & Latched 10

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 11: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

Deployable Masts & Booms • STEM (Storable Tubular Extendible Members)

• Telescopic Tube Mast

• Hinge Products

11

http://www.northropgrumman.com/BusinessVentures/AstroAerospace/Products/Pages/STEM.aspx

http://www.northropgrumman.com/BusinessVentures/AstroAerospace/Products/Pages/TelescopicTubeMasts.aspx

http://www.northropgrumman.com/BusinessVentures/AstroAerospace/Products/Pages/HingesDeployBooms.aspx

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 12: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

STEM™ (Storable Tubular Extendible Member)

STEM

BI-STEM

Interlocking BI-STEM

Benefits Very small stowed package Retractable

SELENE Lunar Sounder Antennas Hubble Solar Array Deployer

JWST Mid-Boom Deployment Actuator

Applications Linear actuators Antennas Deployment drives

Quad-STEM Deployment Actuator

12 Cleared for public release; NGAS Case 14-1846 dated 9/10/14

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ASTRO AEROSPACE

JIB Technology – Stored Energy Deployment

• Self Deploying Monopole • Non-Pyrotechnic Release Mechanization • Any Length Up 25 Feet • 1/2 to 1 3/8 Inch Diameters • Significant Flight Heritage (Over 25

Different Missions, 1000s of Deployments)

Link toHigh Speed Video

Stowed 2 in Length

Deployed 9 ft Length

Link to Full Speed Video

13 Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 14: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

Mars Pathfinder Rover Ramps

Low Mass: 1.0 kg (2.2 lb) Small Stowed Package: 7.6 cm (3.0 in) diameter 42 cm (16.5 in) long Self-Deployed Stable Structure: Supports 12.5 kg (27.6 lb) Rover Provides 136 cm (53.5 in) long ramp

Customer: JPL 14

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 15: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

Telescopic Tube Mast

Lightweight Mast Technology Enables Large Deployables

• Benefits – Modular – Robust design – Can be made from

many materials

JWST Sunshield Boom Development Unit

• Applications – Antenna support

structures – Solar array support

structure – Instrument deployment

boom – Experiment package

support – Nuclear reactor

separation boom – Deployable radiator

boom

15

Link to deployment video

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 16: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

Prototype – Telescopic Tube Mast

• Deployed Length: 110 feet • Stowed Length: 8 feet • Mass: 175 lb • Deployment System: 120-lb-output force STEM

drive • Operation: Deployment and Retraction • 12 Locking pins per tube interface • Light weight thin wall composite tubes

Link to Deployment Video

16 Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 17: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

Telescopic Tube Mast

Boom - Flight Qualified & Safe Man-Rated for the

Space Shuttle Application

Small Compact & Pinless Lightweight Telescopic Tube

Mini- Telescopic Boom • Mini STEM Drive – 15 lbf • Telescopic boom approx 1” dia.

17 Cleared for public release; NGAS Case 14-1846 dated 9/10/14

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ASTRO AEROSPACE

Hinging Mechanisms

• CALM Hinge – Designed for high

stiffness boom deployment

– Low Shock – Retractable

• Hinge Line Deployment – Designed for deployment of

stacked rigid panels – High stiffness joints for high

accuracy arrays – Compact design resides within panel

thickness

• Spring Hinges – Based on Proven

STEM Technology Light flat profile

Many Motorized, Cable Driven, Spring/damper Hinges

18

Link to Video Link to Video

Link to Video

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 19: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

Extendable Support Structure (ESS)

• AstroFold • Custom Designs

19

http://www.northropgrumman.com/BusinessVentures/AstroAerospace/Products/Pages/ExtendibleSupportStructure.aspx

Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 20: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary

ASTRO AEROSPACE

AstroFold – Extendable Support Structure (ESS)

ISAT Proposed SAR Structure

Sequence of Events – Release of launch tie-downs allows

small first motion of truss due to stowed strain energy

– Extension and latch-out of telescoping diagonals

– Secondary restraint is released – Cable spoolers deploy truss in

controlled and synchronized manner – Slack diagonal cords are managed

with devices developed for AstroMesh

– Longeron tensioning cables preload structure to complete deployment

– Truss can be bowed as required by differential longeron tensions

Link to Deployment Video

20 Cleared for public release; NGAS Case 14-1846 dated 9/10/14

Page 21: Astro Aerospace Click Here for Overview Video · PDF fileASTRO AEROSPACE Astro Aerospace 1 Use this space to communicate your key takeaway (or remove) Mark pages according to the proprietary