Akaflieg Berlin B5

{{Short description|German single-seat glider, 1937}}

{{Infobox aircraft begin

| name=B5

| image=

| caption=

}}{{Infobox aircraft type

| type=Sailplane

| national origin=Germany

| manufacturer=Akaflieg Berlin

| designer=

| first flight=1937

| introduced=

| retired=

| status=

| primary user=

| more users=

| produced=

| number built=1

| program cost=

| unit cost=

| developed from=

| variants with their own articles=

}}

The Akaflieg Berlin B5 was a glider built in Germany in the late 1930s. It featured a high-wing, cantilever sailplane configuration of all-wood construction, with cantilevered gull-wings, retractable landing-gear, all-moving-tail, dive air-brakes.{{cite journal |title=Segelflugzeug B 5 |journal=Flugsport |date=August 1937 |issue=16 |pages=416–418. |language=German}}

Specifications (B5)

{{Aircraft specs

|ref=,{{cite book |last1=Wefeld |first1=Hans Joachim |title=75 Jahre 10 NI AKAFLIEG BERLIN 1920 - 1995 |date=1995 |publisher=Akademische Fliegergruppe Berlin e.V. |pages=48–49, 60–61 |language=German }} Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944{{cite book |last=Schneider |first=Helmut (Dipl.Ing.) |title=Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944 |date=1944 |publisher=Herm. Beyer Verlag |location=Leipzig |isbn=381120484X |edition=Facsimile reprint 1986 |language=German |page=282}}

|prime units?=met

|crew=1

|length m=6.15

|span m=15

|height m=1.24

|wing area sqm=11

|wing area note=

  • Length de-rigged: {{cvt|7.28|m|0}}
  • Width de-rigged (without tailplane): {{cvt|1|m|0}}
  • Width de-rigged (with tailplane): {{cvt|2.5|m|0}}
  • Height de-rigged: {{cvt|1.24|m|0}}

|aspect ratio=20.45

|airfoil= root Göttingen 549; mid span Göttingen 497; tip Göttingen 497

|empty weight kg=140

|gross weight kg=225

|max takeoff weight kg=

|more general=

|stall speed kmh=

|stall speed note=

|never exceed speed kmh=228

|never exceed speed note=

  • Aerotow speed: {{cvt|120|km/h|mph kn}}

|g limits=+8 (ultimate)

|glide ratio=30.5:1 at {{cvt|76|km/h|mph kn}}

|sink rate ms=0.67

|sink rate note=at {{cvt|64|km/h|mph kn}}

|lift to drag=

|wing loading kg/m2=20.45

|more performance=

}}

See also

References