MARS EXPLORER ROVER B (27849)

COSPAR: 2003-032A | Alt Name: Opportunity Rover
DECAYED

Image
MARS EXPLORER ROVER B Satellite Image
Additional Sources
Launch Details

Launch Date

July 8, 2003

Launch Pad

SLC17B

Launch Vehicle

Delta 7925H

Orbital Elements

NORAD ID

27849

International Designator

2003-032A

Decay Date

1/25/2004

Basic Satellite Info

Name

MARS EXPLORER ROVER B

Alternative Name

Opportunity Rover

Type

Payload

Status

Decayed

Owner

JPL

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
MARS EXPLORER ROVER B, also known as Opportunity Rover, is an American satellite manufactured by JPL and launched on July 8, 2003, from AFETR SLC17B using a Delta 7925H launch vehicle. It has a length of 1.4 meters, a diameter of 1 meter, and a span of 1.4 meters. The dry mass is 185 kg, which is the same as its launch mass. The satellite's configuration includes a spin-stabilized cruise stage, an airbag-cushioned lander, and a rover. Its power source consists of solar cells and batteries for both the cruise stage and fixed solar arrays with batteries for the rover. The mission purpose was to explore Mars through landing and roving on its surface. It has been operational well beyond its 3-month design lifetime.
Physical Characteristics

Length

1.4

Diameter

1

Span

1.4

Dry Mass

185

Launch Mass

185

Shape

Box + 6 Wheel + 2 Ant

Radar Cross Section

6.2707

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Mars Exploration Rover 1

Purpose

Mars Lander / Rover

Mission

Mars Lander / Rover

Manufacturer

JPL

Life Expectancy

3 month (design), still operational (#2)

Bus

MPF

Configuration

Spin stabilized cruise stage, airbag-cushioned lander, rover

Motor

?

Equipment

see above

Power System

Solar cells, batteries (cruise stage); fixed solar arrays, batteries (rover)

ADCS

Unknown

Transmitter Frequency

Unknown

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