Orbital Overlap TEE Deployer Model 214 Manuale Utente

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Overlap
TEE Deployer
Model 214
Overlap
TEE Deployer
Model 214
Typical Technical Specifications:
Introduction
The Overlap deployer Model 214 was developed for
the German Helios A&B satellites. This motorized
mechanism is capable of extending and retracting a 60
foot (18.3 meter) long Tubular Extendible Element (TEE).
The deployer features electrical stops at full-extend and
–retraction. A potentiometer, driven by the moving
element, provides a continuous indication of deployed
length. This deployment mechanism design will meet the
requirements of document MIL-A-083577B (USAF)
General Specification for Moving Mechanical
Assemblies for Space and Launch Vehicles.
Antenna Element
Deployed Length: Up to 60 feet
(18.3 meters)
Diameter: 0.25 in (0.64 cm)
Configuration: Overlap
Material: Beryllium Copper,
Alloy 25
0.0015 in thick
(0.0381 mm)
Thermal Control Silver with Kapton
Coating: (if required)
Deployer
Height: 2.714 in
(6.894 cm)
Length (Basic): 6.312 in
(16.033 cm)
Width: 4.812 in
(12.223 cm)
Drive Motor: Motor-Inverter
Assembly
Power: 14 Watts maximum
Voltage: 28 Vdc
Deployment Rate: Approximately
0.3 in/sec
(0.76 cm/sec)
Operating
Temperature Range: -30°C to +60°C
Storage
Temperature Range: -55°C to +60°C
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Sommario

Pagina 1 - Introduction

OverlapTEE DeployerModel 214OverlapTEE DeployerModel 214Typical Technical Specifications:IntroductionThe Overlap deployer Model 214 was developed for

Pagina 2 - Features

Orbital Technical Services Division5010 Herzel PlaceBeltsville, MD 20705Phone: (301) 902-1152 FAX: (301) 931-0396www.orbital.com7500 Greenway Ctr. Dr.

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