Apollo AS-202

Overview

Destination: Suborbital
Mission: Test Flight

Suborbital Launch Complex 34 Cape Canaveral SFS, FL, USA

Second uncrewed suborbital test flight of an Apollo CSM with the Saturn IB launch vehicle.

Saturn IB

Family:
Configuration: IB

The Saturn IB (pronounced "one B", also known as the Uprated Saturn I) was an American launch vehicle commissioned by the National Aeronautics and Space Administration (NASA) for the Apollo program. It replaced the S-IV second stage of the Saturn I with the much more powerful S-IVB, able to launch a partially fueled Apollo Command/Service Module (CSM) or a fully fueled Lunar Module (LM) into low Earth orbit for early flight tests before the larger Saturn V needed for lunar flight was ready.

Specifications
  • Stages
    2
  • Length
    43.2 m
  • Diameter
    6.61 m
  • Fairing Diameter
  • Launch Mass
    590.0 T
  • Thrust
    7100.0 kN
Family
  • Name
    Saturn IB
  • Family
  • Variant
    IB
  • Alias
  • Full Name
    Saturn IB
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    21000.0 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Apollo CSM-011


In-active Human Rated Unmanned Crew Capacity: 3 Payload Capacity: 1050 kg
Destination: Suborbital
Serial Number: CSM-011

Apollo CSM used for the AS-202 suborbital test flight.

Apollo Command/Service Module Details

National Aeronautics and Space Administration

National Aeronautics and Space Administration

(NASA)

Acting Administrator: James Free Founded: 1958 Successes: 121 Failures: 20 Pending: 6

Agency Type:

The National Aeronautics and Space Administration is an independent agency of the executive branch of the United States federal government responsible for the civilian space program, as well as aeronautics and aerospace research. NASA have many launch facilities but most are inactive. The most commonly used pad will be LC-39B at Kennedy Space Center in Florida.

INFO WIKI

Cape Canaveral SFS, FL, USA

Launch Complex 34


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