| DOI | Resolve DOI: https://doi.org/10.4224/40003653 |
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| Author | Search for: Bird, J. W.1; Search for: Rudnitski, D. M.1 |
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| Affiliation | - National Research Council Canada. Division of Mechanical Engineering
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| Format | Text, Technical Report |
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| Physical description | 45 p. |
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| Abstract | As part of the stores clearance program of the CRV-7 rocket for carriage on the CF5 aircraft, extensive engine data have been collected during actual rocket firing. These data have been examined to check for rocket exhaust gas ingestion and any associated engine responses. Of the thirty-four sets of engine data examined, seven showed hot gas ingestion which increased the compressor inlet temperature by 2-10°C for a period of 1/2 to 1 second about 2 seconds after firing. In all cases but one, the resulting engine response was consistent with normal operation during temporary increases in inlet temperature. One engine stall occurred and cleared without pilot intervention; it was likely due to ingestion of debris from rockets which disintegrated during launch. With the small sample of missions it was not possible to establish a correlation between delivery parameters, number and location of rockets fired and ingestion of exhaust gases by the engine. |
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| Publication date | 1982-11-10 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Note | The content is temporarily unavailable |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | 13853d1d-39fd-4f23-8c99-680964c35ecb |
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| Record created | 2025-08-26 |
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| Record modified | 2025-11-26 |
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