STS 93 (25866)

COSPAR: 1999-040A | Alt Name: Columbia (STS-93)
DECAYED

Image
STS 93 Satellite Image
Additional Sources
Launch Details

Launch Date

July 23, 1999

Launch Pad

LC39B

Launch Vehicle

Space Shuttle

Orbital Elements

NORAD ID

25866

International Designator

1999-040A

Decay Date

7/28/1999

Basic Satellite Info

Name

STS 93

Alternative Name

Columbia (STS-93)

Type

Payload

Status

Decayed

Owner

JSC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
STS 93 was a Space Shuttle mission flown by Columbia (OV-102) and launched on July 23, 1999, from Launch Pad LC39B at Cape Canaveral Air Force Station using the Space Shuttle as its launch vehicle. The spacecraft has a winged orbiter configuration with dimensions of 37.3 meters in length and span, and a diameter of 23.8 meters. Its dry mass is approximately 89,293 kilograms while it weighed around 95,205 kilograms at launch. Columbia was equipped with fuel cells and batteries for power generation and operated as a crewed spacecraft. The mission's main propulsion system consisted of the Space Shuttle Main Engines (SSME). The satellite's shape is described as a box with two wings and a fin. The primary purpose of STS 93 was to conduct crewed space missions.
Physical Characteristics

Length

37.3

Diameter

23.8

Span

37.3

Dry Mass

89293

Launch Mass

95205

Shape

Box + 2 Wing + Fin

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

OV-102

Purpose

Crewed Spacecraft

Mission

Crewed Spacecraft

Manufacturer

BNAP

Life Expectancy

Unknown

Bus

STS OV

Configuration

Winged orbiter

Motor

SSME

Equipment

Unknown

Power System

Fuel cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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