VEGA 1 BUS (15432)

COSPAR: 1984-125A | Alt Name: Vega-1
DECAYED

Image
VEGA 1 BUS Satellite Image
Additional Sources
Launch Details

Launch Date

December 15, 1984

Launch Pad

LC200/39

Launch Vehicle

Proton-K/D-1

Orbital Elements

NORAD ID

15432

International Designator

1984-125A

Decay Date

Unknown

Basic Satellite Info

Name

VEGA 1 BUS

Alternative Name

Vega-1

Type

Payload

Status

Unknown

Owner

IKI/BABTS

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
The VEGA 1 BUS (also known as Vega-1), designated by NORAD as CAT ID 15432 and OBJECT_ID 1984-125A, was launched on December 15, 1984, from the Tymshchuk site LC200/39 using a Proton-K/D-1 launch vehicle. Built by NPOL for IKI/BABTS, this satellite has dimensions of approximately 4 meters in length and 2.5 meters in diameter with a span of 9 meters. It weighed 3203 kg at launch and had a dry mass of 2500 kg. The VEGA 1 BUS was designed for Venus flyby and Comet Halley flyby missions, equipped with two deployable fixed solar arrays and batteries (for the probe), as well as additional batteries for the lander. Its structure is described as having a flared cylindrical shape plus two panels.
Physical Characteristics

Length

4

Diameter

2.5

Span

9

Dry Mass

2500

Launch Mass

3203

Shape

Flared Cyl + 2 Pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

5VK No. 901

Purpose

Venus flyby, Comet Halley flyby

Mission

Venus flyby, Comet Halley flyby

Manufacturer

NPOL

Life Expectancy

Unknown

Bus

Venera

Configuration

Unknown

Motor

Unknown

Equipment

Unknown

Power System

2 deployable fixed solar arrays, batteries (probe); batteries (lander)

ADCS

Unknown

Transmitter Frequency

Unknown

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