# B-24 & B-25 tail design

**URL:** <https://boards.straightdope.com/t/b-24-b-25-tail-design/99059>\
**Category:** Factual Questions\
**Created:** [March 19, 2002, 5:24pm UTC](https://boards.straightdope.com/t/b-24-b-25-tail-design/99059 "2002-03-19T17:24:48Z")\
**Posts on this page:** 2\
**Page:** 2

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**Author:** ![Kilt-wearin\_man](https://avatars.discourse-cdn.com/v4/letter/k/82dd89/32.png) [@Kilt-wearin\_man](https://boards.straightdope.com/u/Kilt-wearin_man)\
**Post date:** [March 21, 2002, 6:15pm UTC](https://boards.straightdope.com/t/b-24-b-25-tail-design/99059/21 "2002-03-21T18:15:11Z")

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> [@](#):
>
> \*Originally posted by Kamandi \*  
> \*\*
> 
> That’s a good point. On those twin-engined aircraft most of the structure required to carry two fins is already in place. Putting two fins on an F-16 would require a significant weight increase.
> 
> \*\*

Both Joint Strike Fighter candidates (X-35 and X-36) had single engines and double tails. The X-35 is destined to become the F-35 and replace the F-16, F/A-18, AV-8B Harrier, and A-6 Intruder in US and allied service. I’m sure that General Dynamics had a reason for going with a single tail rather than double tails on the F-16, most likely weight and complexity, since the F-16 was intended as an inexpensive, lightweight dogfighter.

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**Author:** ![ElvisL1ves](https://avatars.discourse-cdn.com/v4/letter/e/5daacb/32.png) [@ElvisL1ves](https://boards.straightdope.com/u/ElvisL1ves)\
**Post date:** [March 22, 2002, 3:07pm UTC](https://boards.straightdope.com/t/b-24-b-25-tail-design/99059/22 "2002-03-22T15:07:06Z")

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Fighters are also designed as far as possible to avoid having any inside right-angle intersections, which have the nasty characteristic of reflecting radar beams right back at the sender. The F/A-18, for instance, has the vertical stabilizers canted to each other and at an odd angle to the fuselage top, and forward of the horizontal stabilizers, just for that reason. With a single tail, it’s hard to avoid having a right angle at the fuselage junction, and stealth considerations may outrank weight and drag in the design.

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