DART (28642)

COSPAR: 2005-014A | Alt Name: DART
DECAYED

Image
DART Satellite Image
Additional Sources
Launch Details

Launch Date

April 15, 2005

Launch Site

WRAS

Launch Pad

RW30/12

Launch Vehicle

Pegasus XL/HAPS

Orbital Elements

NORAD ID

28642

International Designator

2005-014A

Decay Date

5/7/2016

Basic Satellite Info

Name

DART

Alternative Name

DART

Type

Payload

Status

Decayed

Owner

MSFC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
The DART (Demonstration for Autonomous Rendezvous Technology) satellite, also known by its OBJECT_ID 2005-014A, was launched on April 15, 2005, from the WRA Launch Site using a Pegasus XL/HAPS launch vehicle. The spacecraft has dimensions of 1.8 meters in length and diameter, with a span of 1.8 meters as well. It carries an Advanced Video Guidance Sensor (AVGS) as its primary equipment for technology demonstrations related to automatic rendezvous. DART was manufactured by OSCC and owned by MSFC, equipped with batteries for power supply. The satellite's dry mass is 300 kilograms, while its launch mass is 350 kilograms. It operated for only one day post-launch, showcasing its short operational lifetime dedicated to testing autonomous rendezvous technology in space.
Physical Characteristics

Length

1.8

Diameter

1

Span

1.8

Dry Mass

300

Launch Mass

350

Shape

Step Cyl

Radar Cross Section

1.11

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

HAPS 8

Purpose

Technology, automatic rendezvous

Mission

Technology, automatic rendezvous

Manufacturer

OSCC

Life Expectancy

1 day

Bus

HAPS

Configuration

Equipment mounted on HAPS stage

Motor

HAPS

Equipment

AVGS (Advanced Video Guidance Sensor)

Power System

Batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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