Subsystem Technology and Design Library

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Contents

General References

  • NASA Space Vehicle Design Criteria, SP-8000 Good introductory references for spacecraft subsystem and mission design; may be somewhat outdated with regard to specific technologies due to publication dates (1960s and 1970s)


Structures

Inflatable Habitat Structures

Mechanisms


Propulsion

Chemical Propulsion

Advanced Propulsion

General Electric Propulsion

General Nuclear Propulsion

Nuclear Thermal Propulsion

Nuclear Electric Propulsion (NEP)

Solar Electric Propulsion

Under construction...

Nuclear Pulse Propulsion

Nuclear pulse propulsion as a means of achieving very high specific impulses (several thousand s) and high thrust at the same time was explored extensively during the 1950s and 1960s as part of Project Orion in the United States. Potential applications of nuclear pulse propulsion systems included human exploration of all parts of the solar system. The following documents provide an overview of the technical capabilities of nuclear pulse propulsion systems:

Solar Sailing

Conceptual Future Propulsion


Electrical Power System (EPS)

The EPS provides the functions: electrical power generation, storage, management, and distribution.

General EPS references

EPS Design Studies

Mars Surface Power System Design Studies

Primary and Secondary Battery Systems

Photovoltaic Power Generation

Radioisotope Power Generation

Fission Power Generation

Fuel Cell Systems

Thermal Control (TC)

Environmental Control & Life Support System (ECLSS)

General ECLSS References

  • US Navy Diving Manual - Volume 1: Air Diving, NAVSEA 0994-LP-001-9010, Revision 1, June 1985, Navy Department Washington, D.C.

ECLSS Technologies

Atmosphere Revitalization

Water Management

Food Management

Waste Management

Under construction...

Atmosphere Thermal Conditioning

Under construction...

Integrated ECLSS Design Studies / Tests

Crew Systems

Avionics / Astrionics


Guidance, Navigation & Control (GN&C)

Entry, Descent & Landing (EDL)

  • NASA Technical Note D-4098 [Harris, August 1967] Aerodynamic Characteristics of a Spherically Blunted 25 Degree Cone at a Mach Number of 20
  • Mars Exploration Entry, Descent and Landing Challenges (PDF) [Braun RD, Manning RM, 2006] Excellent paper providing an overview of existing Mars EDL systems and technology (primarily based on Viking heritage), limitations to extending this technology, and a summary of the challenges for human-scale Mars EDL.
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