This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
CONCURRENT DESIGN OF ENGINES AND SPECIFICATIONS OF STARTING SYSTEMS FOR HELICOPTERS
- Aerospace Standard
- AIR1296
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
It is recommended that all helicopter engine development programs include an evaluation of engine starting requirements. The evaluation should include starting requirement effects on helicopter weight, cost, and mission effectiveness. The evaluation should be appropriate to the engine stage of development.
Data Sets - Support Documents
No Datasets Available
Issuing Committee
S-12 Powered Lift Propulsion Committee
Provides guidance and standardization for the better utilization of helicopter powerplants through studies of current practices in engine design, engine/airframe interface, and engine operation.
For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright, and Membership" link in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.Reference
| Number | Title |
|---|
* Redlines comparisons are available for those standards
listed in the Revision History that contain a radio button. A
redline comparison of the current version against a revision is
accomplished by selecting the radio button next to the standard and
then selecting 'compare'. At this time, Redline versions only exist
for some AMS standards. SAE will continue to add redline versioning
with ongoing updates to SAE MOBILUS.