2012Unpublished venueRequires access

Radiation Exposures for Commercial Deep Space Missions: EM/L1, Lunar and NEO Scenarios

Bill Atwell

Open publisher page 0 citations

Abstract

Radiation exposures to humans and onboard electronics systems are a major concern for commercial deep space missions, especially those mission scenarios that entail long durations. There are some mission planning considerations being given to use the EarthMoon libration point 1 (EM/L1) as an operations base for propellant depots and for staging missions to the Moon and Near Earth Objects (NEOs). These missions will subject crews and spacecraft systems to two sources of space radiation: the extremely energetic galactic cosmic radiation (GCR) and solar proton events (SPEs). Both of these radiation sources vary with the so-called 11-year solar cycle. The GCR environment, although at a low particle flux level, represents long-term biological effects to humans and short-term effects to onboard systems. Large solar proton events represent the single-most important source of acute space radiation exposure to humans and radio-sensitive spacecraft systems for deep space missions. In this paper, radiation exposures to humans and onboard systems are presented for several baseline design reference missions: the free-space environment for EM/L1, lunar surface, and NEO missions. For lunar surface and NEO missions the radiation exposures are approximately one-half the free-space exposures. The crew radiation exposures for each mission scenario are compared with the current astronaut radiation exposure limits. In addition, radiation effects on spacecraft systems, especially electronics, are discussed in detail.

About this research paper

What this paper is about

Radiation exposures to humans and onboard electronics systems are a major concern for commercial deep space missions, especially those mission scenarios that entail long durations. There are some mission planning considerations being given to use the EarthMoon libration point 1 (EM/L1) as an operations base for propellant depots and for staging missions to the Moon and Near Earth Objects (NEOs). These missions will subject crews and spacecraft systems to two sources of space radiation: the extremely energetic galactic cosmic radiation (GCR) and solar proton events (SPEs). Both of these radiation sources vary with the so-called 11-year solar cycle. The GCR environment, although at a low particle flux level, represents long-term biological effects to humans and short-term effects to onboard systems. Large solar proton events represent the single-most important source of acute space radiation exposure to humans and radio-sensitive spacecraft systems for deep space missions. In this paper, radiation exposures to humans and onboard systems are presented for several baseline design reference missions: the free-space environment for EM/L1, lunar surface, and NEO missions. For lunar surface and NEO missions the radiation exposures are approximately one-half the free-space exposures. The crew radiation exposures for each mission scenario are compared with the current astronaut radiation exposure limits. In addition, radiation effects on spacecraft systems, especially electronics, are discussed in detail.

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Radiation exposures to humans and onboard electronics systems are a major concern for commercial deep space missions, especially those mission scenarios that entail long durations. There are some mission planning considerations being given to use the EarthMoon libration point 1 (EM/L1) as an operations base for propellant depots and for staging missions to the Moon and Near Earth Objects (NEOs). These missions will subject crews and spacecraft systems to two sources of space radiation: the extremely energetic galactic cosmic radiation (GCR) and solar proton events (SPEs). Both of these radiation sources vary with the so-called 11-year solar cycle. The GCR environment, although at a low particle flux level, represents long-term biological effects to humans and short-term effects to onboard systems. Large solar proton events represent the single-most important source of acute space radiation exposure to humans and radio-sensitive spacecraft systems for deep space missions. In this paper, radiation exposures to humans and onboard systems are presented for several baseline design reference missions: the free-space environment for EM/L1, lunar surface, and NEO missions. For lunar surface and NEO missions the radiation exposures are approximately one-half the free-space exposures. The crew radiation exposures for each mission scenario are compared with the current astronaut radiation exposure limits. In addition, radiation effects on spacecraft systems, especially electronics, are discussed in detail.

Key concepts: Astrobiology, NASA Deep Space Network, Remote sensing, Aerospace engineering, Space exploration, Space (punctuation), Environmental science, Deep space exploration

Related papers

Back to paper searchBrowse research topicsOriginal source
Radiation Exposures for Commercial Deep Space Missions: EM/L1, Lunar and NEO Scenarios — Research Paper | ScholarLens