SHENZHOU-5 (SZ-5) (28043)

COSPAR: 2003-045A | Alt Name: Shenzhou 5
DECAYED

Image
SHENZHOU-5 (SZ-5) Satellite Image
Additional Sources
Launch Details

Launch Date

October 15, 2003

Launch Site

JSC

Launch Pad

LC921

Launch Vehicle

Chang Zheng 2F

Orbital Elements

NORAD ID

28043

International Designator

2003-045A

Decay Date

10/16/2003

Basic Satellite Info

Name

SHENZHOU-5 (SZ-5)

Alternative Name

Shenzhou 5

Type

Payload

Status

Decayed

Owner

CMSEO

Country

China

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
SHENZHOU-5 (SZ-5), also known as Shenzhou 5, is a crewed spacecraft launched on October 15, 2003, from Jiuquan Satellite Launch Center (JSC) using the Chang Zheng 2F launch vehicle. The spacecraft consists of a service module, return module, and autonomous orbital module and was manufactured by CALT for China's Manned Space Engineering Office (CMSEO). SHENZHOU-5 has dimensions of 10 meters in length, 3.2 meters in diameter, and spans 10 meters across its solar arrays. It weighs 3,300 kilograms at launch and is equipped with four deployable solar arrays for power generation alongside batteries. The mission's purpose was to support crewed spaceflight operations, and it utilized a configuration of cylindrical and conical segments.
Physical Characteristics

Length

10

Diameter

3.2

Span

10

Dry Mass

3300

Launch Mass

3300

Shape

Cyl + Cone + Cyl

Radar Cross Section

10.0237

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Shenzhou 5 Fanhui Cang

Purpose

Crewed spacecraft

Mission

Crewed spacecraft

Manufacturer

CALT

Life Expectancy

Unknown

Bus

Shenzhou

Configuration

Service module, Return module, Autonomous orbital Module

Motor

4 x retro motors

Equipment

Unknown

Power System

4 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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