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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{{Infobox Aircraft
{|{{Infobox aircraft begin
|name = CG-15 "Waco"
|name= CG-15
|image= File:Waco CG-15A.jpg
|type = [[Military glider]]
|caption= CG-15A
|manufacturer = [[WACO|Waco Aircraft Company]]
}}{{Infobox aircraft type
|image =
|type=[[Military glider]]
|caption =
|national origin= United States
|designer =
|manufacturer=[[Waco Aircraft Company]]
|first flight =
|designer=
|introduction =
|first flight=
|retired =
|introduction=
|status =
|retired=
|primary user = [[United States Army Air Forces|US Army Air Forces]]
|status=
|more users =
|primary user=[[United States Army Air Forces]]
|produced =
|more users=
|number built = 427
|produced=
|unit cost =
|number built=473
|variants with their own articles = [[CG-4A Waco]]
|unit cost=
|developed from= [[Waco CG-4]]
|variants with their own articles=
}}
}}
|}
The '''CG-15 Waco''' was [[Military glider]] developed from the [[CG-4A Waco]]. Although outwardly similar to the earlier CG-4, and carrying the same number of passengers, a number of changes in the design, including shortened wings and a more streamlined nose enabled it to travel faster. 1,000 were ordered and 473 were delivered before production ceased. Two were transferred to the Navy for testing as the XLR2W-1. One of the aircraft was converted into a XPG-3 powered glider which used two Jacobs R-755-9 radial engines.

The '''Waco CG-15''' was an American [[military glider]], which was developed from the [[Waco CG-4|CG-4]]. Although outwardly similar to its predecessor and carrying the same number of passengers, a number of changes in the design, including shortened wings and a more streamlined nose enabled it to travel faster. 1,000 were ordered and 473 were delivered before production ceased. Two were transferred to the Navy for testing as the XLR2W-1. One unit was converted into an XPG-3 powered glider which used two [[Jacobs R-755|Jacobs R-755-9]] radial engines.

==Variants==
;'''XCG-15''':Prototype converted from a [[CG-4 Waco|CG-4A]], one conversion.
;'''XCG-15A''':New-build prototypes, two built.
;'''CG-15A''':Production variant, redesignated G-15A in 1948, 427 built.
;'''PG-3''':One XCG-15A fitted with two R-755-9 engines, redesignated G-3A in 1948.
;'''XLR2W-1''':Two CG-15As transferred to the [[United States Navy]].
;'''G-3A''':PG-3 redesignated in 1948.
;'''G-15A''':CG-15A redesignated in 1948.


==Operators==
==Operators==
;{{flag|United States|1912}}:
;{{flag|United States|1912}}:
*[[US Army Air Force]]
* [[United States Army Air Force]]
*[[US Navy]]
* [[United States Navy]]


==Specifications (CG-15A)==
==Specifications (CG-15A)==

{{aircraft specifications
{{Aircraft specs
|plane or copter?=plane
|ref=Fighting Gliders of World War II<ref name=Mrazek>{{cite book |last1=Mrazek |first1=James E. |title=Fighting Gliders of World War II |publisher=St. Martin's Press |location=London |isbn=978-0-312-28927-0 |edition=1st |date=1 January 1977 |url=https://archive.org/details/fightinggliderso00mraz |pages=130-133}}</ref>
|jet or prop?=neither
|prime units?=imp
|ref=
<!--
|crew=two, pilot and co-pilot
General characteristics
|capacity=
-->
|payload main=
|crew=2 pilots
|payload alt=
|capacity=13 troops / {{cvt|4035|lb|0}}
|length main= 48 ft 10 in
|length alt= 14.9 m
|length ft=48
|length in=9.6
|span main= 62 ft 2 in
|length note=
|span alt= 18.95 m
|span ft=62
|height main=
|span in=1.2
|height alt=
|span note=
|area main= 623 ft²
|height ft=12
|area alt= 57.88 m²
|height in=8.4
|airfoil=
|height note=<br>
|empty weight main= 4,000 lb
*'''Cargo compartment:'''
|empty weight alt= 1,800 kg
:*'''Length:''' {{cvt|13|ft|1.2|in|1}}
|loaded weight main=
:*'''Width:''' {{cvt|5|ft|10.2|in|1}}
|loaded weight alt=
:*'''Height:''' {{cvt|5|ft|6|in|1}}
|useful load main=
|wing area sqft=623
|useful load alt=
|wing area note=
|max takeoff weight main=8,035 lb
|aspect ratio=6.21
|max takeoff weight alt= 3,640 kg
|airfoil=[[NACA airfoil|NACA 43012]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019}}</ref>
|empty weight lb=4000
|empty weight note=
|gross weight lb=8035
|gross weight note=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|more general=
<!--
|max speed main=180 mph
Performance
|max speed alt= 290 km/h
-->
|cruise speed main=
|cruise speed alt=
|cruise speed mph=
|stall speed main=
|cruise speed note=
|stall speed alt=
|stall speed mph=62
|never exceed speed main=
|stall speed note=flaps up
::::{{cvt|53|mph|kn km/h|0}} flaps down
|never exceed speed alt=
|never exceed speed mph=180
|range main=
|never exceed speed note=<br>
|range alt=
::::{{cvt|100|mph|kn km/h|0}} with flaps lowered
|ceiling main=
|glide ratio=
|ceiling alt=
|climb rate main=
|sink rate ftmin=<!-- sailplanes -->
|climb rate alt=
|sink rate note=
|lift to drag=
|loading main=
|loading alt=
|wing loading lb/sqft=12.9
|wing loading note={{Citation needed|date=August 2020}}
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
|armament=
|avionics=
}}
}}
{{aero-specs}}


==References==
==See also==
* {{cite web
| url = http://www.fiddlersgreen.net/AC/aircraft/WACO-cg4/waco_info/info.php
| title = The WACO CG-4A Invasion Glider
| accessdate = 30 April
| accessyear = 2007
| last =
| first =
| work = Fiddlersgreen.net
}}
* {{cite web
| url = http://www.daveswarbirds.com/usplanes/aircraft/cg-15a.htm
| title = WACO CG-15A
| accessdate = 30 April
| accessyear = 2007
| last = Handon
| first = David
| work = Dave's warbirds.com
}}

<references/>

==Related content==
{{aircontent|
{{aircontent|
|related=
|related=
[[CG-4A Waco]]
*[[Waco CG-4A]]

|similar aircraft=
|similar aircraft=
*[[Airspeed Horsa]]
*[[Airspeed Horsa]]
*[[Slingsby Hengist]]
*[[General Aircraft Hamilcar]]
*[[General Aircraft Hotspur]]
*[[DFS 230]]
*[[DFS 230]]
*[[General Aircraft Hamilcar]]
*[[General Aircraft Hotspur]]
*[[Gotha Go 242]]
*[[Gotha Go 242]]
*[[Schweizer cargo glider designs]]
*[[Slingsby Hengist]]
|lists=
*[[List of aircraft of World War II]]
*[[List of World War II military gliders]]
|see also=
}}


==References==
|sequence=
{{Reflist}}
|lists=[[List of World War II military gliders]]
*{{cite web|url=http://www.fiddlersgreen.net/models/Aircraft/WACO-CG-4.html|title=Fiddlersgreen paper model of WACO CG-4 Invasion Glider with historical notes and photos}}
*{{cite web|url=http://www.daveswarbirds.com/usplanes/aircraft/cg-15a.htm|title=WACO CG-15A|access-date=30 April 2007|last=Handon|first=David|work=Dave's warbirds.com}}


{{Waco aircraft}}
|see also=
{{US glider aircraft}}
}}
{{USN glider aircraft}}


{{DEFAULTSORT:Waco Cg-15}}
[[Category:Glider aircraft]]
[[Category:U.S. military transport aircraft 1940-1949]]
[[Category:1940s United States military transport aircraft]]
[[Category:World War II aircraft]]
[[Category:World War II aircraft of the United States]]
[[Category:1940s United States military gliders]]
[[Category:Waco aircraft|CG-15]]

Latest revision as of 22:54, 2 January 2021

CG-15
CG-15A
Role Military glider
National origin United States
Manufacturer Waco Aircraft Company
Primary user United States Army Air Forces
Number built 473
Developed from Waco CG-4

The Waco CG-15 was an American military glider, which was developed from the CG-4. Although outwardly similar to its predecessor and carrying the same number of passengers, a number of changes in the design, including shortened wings and a more streamlined nose enabled it to travel faster. 1,000 were ordered and 473 were delivered before production ceased. Two were transferred to the Navy for testing as the XLR2W-1. One unit was converted into an XPG-3 powered glider which used two Jacobs R-755-9 radial engines.

Variants[edit]

XCG-15
Prototype converted from a CG-4A, one conversion.
XCG-15A
New-build prototypes, two built.
CG-15A
Production variant, redesignated G-15A in 1948, 427 built.
PG-3
One XCG-15A fitted with two R-755-9 engines, redesignated G-3A in 1948.
XLR2W-1
Two CG-15As transferred to the United States Navy.
G-3A
PG-3 redesignated in 1948.
G-15A
CG-15A redesignated in 1948.

Operators[edit]

 United States

Specifications (CG-15A)[edit]

Data from Fighting Gliders of World War II[1]

General characteristics

  • Crew: 2 pilots
  • Capacity: 13 troops / 4,035 lb (1,830 kg)
  • Length: 48 ft 9.6 in (14.874 m)
  • Wingspan: 62 ft 1.2 in (18.928 m)
  • Height: 12 ft 8.4 in (3.871 m)
  • Cargo compartment:
  • Length: 13 ft 1.2 in (4.0 m)
  • Width: 5 ft 10.2 in (1.8 m)
  • Height: 5 ft 6 in (1.7 m)

Performance

  • Stall speed: 62 mph (100 km/h, 54 kn) flaps up
53 mph (46 kn; 85 km/h) flaps down
100 mph (87 kn; 161 km/h) with flaps lowered

See also[edit]

Related development

Aircraft of comparable role, configuration, and era

Related lists

References[edit]

  1. ^ Mrazek, James E. (1 January 1977). Fighting Gliders of World War II (1st ed.). London: St. Martin's Press. pp. 130–133. ISBN 978-0-312-28927-0.
  2. ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.