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Introduction: the challenge of optimum integration of propulsion systems and large space structures
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carlisle, R. F. |
| Copyright Year | 1980 |
| Description | A functional matrix of possible propulsion system characteristics for a spacecraft for deployable and assembled spacecraft structures shows that either electric propulsion or low thrust chemical propulsion systems could provide the propulsion required. The trade-off considerations of a single propulsion engine or multiengines are outlined and it is shown that a single point engine is bounded by some upper limit of thrust for assembled spacecraft. The matrix also shows several additional functions that can be provided to the spacecraft if a propulsion system is an integral part of the spacecraft. A review of all of the functions that can be provided for a spacecraft by an integral propulsion system may result in the inclusion of the propulsion for several functions even if no single function were mandatory. Propulsion interface issues for each combination of engines are identified. |
| File Size | 278983 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800022944 |
| Archival Resource Key | ark:/13960/t6c29q53b |
| Language | English |
| Publisher Date | 1980-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Interfaces Electric Propulsion Mass Drivers Low Thrust Propulsion Attitude Control Space Missions Systems Engineering Payload Delivery Sts Propulsion System Configurations Chemical Propulsion Spacecraft Propulsion Large Space Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
