Kaman K-700
Script error: No such module "AfC submission catcheck".
Some of this article's listed sources may not be reliable. (June 2022) (Learn how and when to remove this template message) |
| Kaman K-700 | |
|---|---|
| Role | Helicopter |
| National origin | United States of America |
| Designer | Kaman |
The Kaman K-700 was a proposed rescue helicopter built by Kaman. It was designed in 1969 for the United States Air Force. It employed the use of two PT6A turboshafts, streamlined fuselage and a large tail fin. However, it never progressed past the design stage.[1][2]
Design and development[edit]
The aircraft was designed to hold a maximum of 14 passengers. It had a stretched fuselage of approximately 12.5 m. In addition, the K-700 was to have a bullet-resistant windshield, self-sealing fuel tanks, provisions for auxiliary tanks, and an array of armament comparable to some contemporary gunships.
The USAF declined to purchase the K-700 even after Kaman's promise to deliver it in under 20 months.[3]
References[edit]
- ↑ Heliport Design Guide. Department of Transportation, Federal Aviation Administration, Airports Service. 1969. pp. 4, 14, 63, 64. Search this book on
- ↑ UC Southern Regional Library Facility (1969). Flight International. 95. United Kingdom: Illiffe Transport Publications. Search this book on
- ↑ "Kaman K-700 helicopter - development history, photos, technical data". www.aviastar.org. Retrieved 2022-03-19.
 | This aircraft-related article is a stub. You can help EverybodyWiki by expanding it. |
This article "Kaman K-700" is from Wikipedia. The list of its authors can be seen in its historical and/or the page Edithistory:Kaman K-700. Articles copied from Draft Namespace on Wikipedia could be seen on the Draft Namespace of Wikipedia and not main one.
