Apollo command and service module and lunar module environmental control systems
The environmental control systems and system requirements of the Apollo command service module and the lunar module are described. The overall performance of both systems during the Apollo program is discussed. Other topics covered include: dust control, EVA provisions, Apollo 13 emergency, component redundancy, modular construction, and subatmospheric design.
Related Apollo Documents
A Flexible Lunar Architecture for Exploration (FLARE) Supporting NASA’s Artemis Program
The Flexible Lunar Architecture for Exploration (FLARE) is a concept to deliver four crew to the lunar surface for a minimum of seven days and then return them safely to Earth. FLARE can be implemente
A historical overview of the electrical power systems in the US manned and some US unmanned spacecraft
A historical overview of electrical power systems used in the U.S. manned spacecraft and some of the U.S. unmanned spacecraft is presented in this investigation. A time frame of approximately 25 years
A Notional Artemis Lunar Surface Exploration Package (ArLSEP) based on the Gandalf Staff Platform
Introduction: The Artemis program is planning to deliver crew and cargo to the lunar surface, but there is no current package for supporting lunar in-struments and experiments similar to the Apollo L