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A project of spacecraft covers a wide region, to include unmanned spacecraft design (satellites and planetary probes), and manned ballistic capsule project (spaceships and space stations). A project & engineering of space vehicle is somewhat related that of rockets and missiles. An crucial difference though is that ballistic capsule work a share or even tons of their life around vacuum & interplanetary space environment.

Ballistic capsule project will bring together aspects of various techniques & technologies, that is to say:

Astronautics for mission project & derivation of the design requirements, Systems engineering for maintaining the project baseline & derivation of subsystem requirements, said subsystems listed following: Telemetry, Telecommand, and Communications (TTC) subsystem, which utilizes technologies & techniques of terrestrial radio and digital communications to communicate with a ground, In-Board Information Treating (OBDH) subsystem, which includes in-board computers and computer buses. Once more this subsystem is according to terrestrial technologies, Software which runs all the in-board applications & as well on line-subordinate software program. This subsystem is very similar to terrestrial real-period & embedded computer software designs, Electrical subsystem, which generates, places & distributes a electrical power to all the on-board equipments, Attitude and Orbit Control (AOCS) subsystem, which uses control theory to point a ballistic capsule right, & maintaaround or even vary a orbit based on data from a mission profile; Although a techniques within AOCS project come park by using terrestrial methods, the devices utilized for propulsion & sensing in space is ordinarily super specific to ballistic capsule, Thermal Control subsystem, which maintains environmental conditions compatible by owning operations of the space vehicle equipments; This subsystem has super space-specific technologies, since within space, radiation and conduction usually dominate as thermal results, by opposition by using Globe in which convection is typically a independent of these, Propulsion subsystem, which provides means of transporting a ballistic capsule from either a single orbit to an additional. This is the exclusively technology which is really specific to space vehicle project. Popular culture has mass produced the cliche of spacecraft propulsion engineers, every bit embodied per term rocket science, Mechanical and Structure subsystem, which addresses a structural components & mechanisms inside the ballistic capsule configuration. These include e.g. beams, panels, & deployable appendages or even separation equipment (to eject from either a launcher rocket).

Ballistic capsule project was innate as a discipline in a 50s & 60s sustaining the advent of U.s. & Russian space exploration programs. Since so it has progressed, although occasionally to a lesser degree corresponding terrestrial technologies.

JPL Part Reliablility
Guidelines for parts selection and space reliability.COTS parts used in Space applications.

Association RADECS
RADiation and its Effect on Components and Systems. Updated information about RADECS association and RADECS conferences will be available on this site in English.

NASA Lessons Learned
NASA Lessons Learned Information System. Appears access is restricted to NASA and approved contractors.

Space Design Links
Links on satellite cost, thermal and environmental design.

Cosmos 1: the first solar sail
The Planetary Society is developing a privately funded solar sail project with Cosmos Studios. The spacecraft will be developed, launched and operated in Russia.

Communications Satellite Software
SATSOFT is used for communication satellite antenna design, analysis, and coverage planning. Quickly assess antenna coverage and gain, conduct antenna sizing studies, develop shaped beam and multibeam antenna designs, and perform other satellite payload engineering tasks.

Discovery Program Documents
Discovery guidelines and requirements documents. Good reference collection.

Laboratory for Spacecraft and Mission Design
A laboratory of the California Institute of Technology dedicated to developing low cost conceptual spacecraft design tools for concurrent space systems engineering.

GAO Space
Description of GAO Associates plus source of free code for space applications and support for aerospace.

Radiation-effects.com
Provide radiation effects services including measurements, data analysis, environment defintion, and technology assessment for space applications.






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