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Fire extinguishing apparatus having a slidable mass for a penetrator nozzle. [for penetrating aircraft and shuttle orbiter skin
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bolton, P. N. Gray, N. C. Senseny, R. M. |
| Copyright Year | 1980 |
| Description | A fire extinguishing apparatus for delivering an extinguishing agent through a tarrier surrounding a structure into its interior includes an elongated tubular nozzle body which has a pointed penetrating head carried on one end of the tubular body. A source of extinguishing agent coupled to the opposite end of the tubular body is fed through and passes through passages adjacent the head for delivering the extinguishing agent to the interior of the structure. A slidable mass is carried on the tubular body on a remote end of the tubular body from the penetrating head. By manipulating the slidable mass and bringing such in contact with an abutment the force imparted to the tubular body causes the head to penetrate the structure. |
| File Size | 308798 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810005625 |
| Archival Resource Key | ark:/13960/t1sf7kg90 |
| Language | English |
| Publisher Date | 1980-08-26 |
| Access Restriction | Open |
| Subject Keyword | Fire Extinguishers Nozzle Geometry Spray Nozzles Penetration Sleeves Pressure Heads Skin Structural Member Axial Loads Sliding Mechanical Devices Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
