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Helicopter payload gains utilizing water injection for hot day power augmentationAn analytical investigation was undertaken to assess the gains in helicopter mission payload through the use of water injection to produce power augmentation in an altitude-hot day environment. Substantial gains are shown for two representative helicopters, the UH-lH and CH-47B. The UH-lH payload increased 86.7 percent for a 50 n.mi. (92.6 km) radius mission involving two out-of-ground effect (OGE) hover take-offs of 2 minutes each at 5000 ft. (1525 m) 35 C ambient conditions. The CH-47B payload increased 49.5 percent for a 50 n.mi. (92.6 km) radius mission with sling loaded cargo as the outbound payload and a 3000 lb. (1360 kg) internal cargo on the return leg. The mission included two 4 min. OGE hovers at 6000 ft. (1830 m) 35 C. An improvement in take off performance and maximum performance climb also resulted as a consequence of the OGE hover capability and higher maximum power available.
Document ID
19720025377
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stroub, R. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62195
Report Number: NASA-TM-X-62195
Accession Number
72N33027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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