Apollo 5

Overview

Destination: Low Earth Orbit
Mission: Human Exploration

Low Earth Orbit Space Launch Complex 34 Cape Canaveral, FL, USA

The Apollo 5 mission tested the Lunar Module in a space environment, in particular its descent and ascent engine systems, and its ability to separate the ascent and descent stages. The descent engine would become the first throttleable rocket engine fired in space.

Saturn IB

Family: Saturn
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 T
  • Thrust
    7100 kN
Family
  • Name
    Saturn IB
  • Family
    Saturn
  • Variant
    IB
  • Alias
  • Full Name
    Saturn IB
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    21000 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

National Aeronautics and Space Administration

Circle Image
Administrator: Jim Bridenstine Founded: 1958 Successes: 38 Failures: 3 Pending: 8

Agency Type: Government

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, FL, USA

Pad: Space Launch Complex 34


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