Loading...
Please wait, while we are loading the content...
Similar Documents
Conceptual design of liquid droplet radiator shuttle-attached experiment technical requirements document
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pfeiffer, Shlomo L. |
| Copyright Year | 1989 |
| Description | The technical requirements of a shuttle-attached Liquid Droplet Radiator (LDR) experiment are discussed. The Liquid Droplet Radiator is an advanced lightweight heat rejection concept that can be used to reject heat from future high powered space platforms. In the LDR concept, submillimeter sized droplets are generated, pass through space, and radiate heat before they are collected and recirculated back to the heat source. The LDR experiment is designed to be attached to the shuttle longeron and integrated into the shuttle bay using standard shuttle/experiment interfaces. Overall power, weight, and data requirements of the experiment are detailed. Shuttle integration and safety design issues are discussed. An overview of the conceptual design of the experiment is presented. Details of the conceptual design are not discussed here, but rather in a separate Final Report. |
| File Size | 1138754 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900002490 |
| Archival Resource Key | ark:/13960/t8md3ts22 |
| Language | English |
| Publisher Date | 1989-10-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Spacecraft Radiators Space Shuttle Payloads Experiment Design Waste Heat Requirements Waste Energy Utilization Heat Transfer Drops Liquids Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
