VENUS EXPRESS (28901)

COSPAR: 2005-045A | Alt Name: Venus Express

DECAYED

Image

Additional Sources

Launch Details

Launch Date

November 9, 2005

Launch Site

Tyuratam Missile and Space Complex

Launch Pad

LC31

Launch Vehicle

Soyuz-FG

Orbital Elements

NORAD ID

28901

International Designator

2005-045A

Decay Date

Unknown

Basic Satellite Info

Name

VENUS EXPRESS

Alternative Name

Venus Express

Type

Payload

Status

Non-operational

Owner

ESA

Country

European Space Agency

Constellation

N/A

Related Satellites

Major Events

N/A

Summary

VENUS EXPRESS, also known as Venus Express, is an ESA satellite designed as a Venus orbiter and based on the Mars Express bus configuration. Launched on November 9, 2005, from TYMSC LC31 using a Soyuz-FG launch vehicle, the spacecraft has dimensions of 1.5 meters in length, 1.8 meters in diameter, and an 8-meter span. The dry mass is recorded at 670 kilograms with a launch mass of 1240 kilograms. Manufactured by EADSB, VENUS EXPRESS utilizes two deployable solar arrays for power along with batteries. The satellite's shape consists of a box configuration augmented by two panels. It was designed and operated under the auspices of ESA, aimed at conducting detailed studies of Venus from orbit.

Physical Characteristics

Length

1.5

Diameter

1.8

Span

Dry Mass

670

Launch Mass

1240

Shape

Box + 2 Pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Venus Express

Purpose

Venus orbiter

Mission

Venus orbiter

Manufacturer

EADSB

Life Expectancy

Unknown

Bus

Rosetta

Configuration

Mars Express bus

Motor

S400-12

Equipment

Unknown

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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