Orbital Overlap TEE Deployer Model 214 Manual do Utilizador descarregar pdf

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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Introduction 1
Features 2

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Página 1 - Introduction

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

Página 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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Orbital Overlap TEE Deployer Model 214 Manual do Utilizador

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