| Název: Name: | KT-04 | KT-04 |
| Originální název: Original Name: | KT-04 | |
| Kategorie: Category: | bezpilotní cílový letoun | target drone |
| Výrobce: Producer: | DD.MM.1974-DD.MM.1985 Rudý Letov n.p., Praha | |
| Období výroby: Production Period: | DD.MM.1974-DD.MM.1985 | |
| Vyrobeno kusů: Number of Produced: | ? | |
| První vzlet: Maiden Flight: | DD.MM.1971 | |
| Základní charakteristika: Basic Characteristics: | ||
| Vzlet a přistání: Take-off and Landing: | konvenční vzlet, přistání na padáku | conventional take-off, landing on a parachute |
| Uspořádání křídla: Arrangement of Wing: | jednoplošník | monoplane |
| Uspořádání letounu: Aircraft Concept: | bezocasé | tailless |
| Podvozek: Undercarriage: | odhazovací | jettisonable |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 110 kg | 243 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 2301) kg | 5071) lb |
| Rozpětí: Wingspan: | 5,00 m | 16 ft 4 ⅞ in |
| Délka: Length: | 4,90 m | 16 ft ⅞ in |
| Výška: Height: | 1,20 m | 3 ft 11 ¼ in |
| Plocha křídla: Wing Area: | 3,00 m2 | 32.29 ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | žádný | none |
| Počet motorů: Number of engines: | 0 | |
| Typ: Type: | - | - |
| Objem palivových nádrží: Fuel Tank Capacity: | - | - |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 6002) km/h v ? m | 3732) mph in ? ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Operační dostup: Service Ceiling: | 2500 m | 8202 ft |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Vytrvalost: Endurance: | 1,33 h | |
| Výzbroj: Armament: | - | - |
| Vybavení: Equipment: | - | - |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | 1) s podvozkem 2) maximální vlečná rychlost | 1) with wheels 2) max tow speed |
| Zdroje: Sources: | Krouhlík, Jiří. Znají je u celého letectva, L+K 1978/19. Havel, Jiří. Vlečný terč KT-04 v akci. L+K 2008/1. Kbely, popiska k exponátu | |
KT-04
vlečený terč
KT-04
Towed target KT-04 was part of the training complex of aircraft L-39. Was vlekán aircraft L-39V. Target is all-metal with samonosným wing. Has SOP, VOP does not. The hull has three parts. In the front is zavěsné devices for connecting ropes, landing parachute, the mechanism of its opening, electric control system and battery. Under the middle part is composed of an inflatable bag for a cushion landing and two curtains for the ejection of the chassis. Inside is a pneumatic installation with a bottle of compressed air for inflating amortizátoru (buffer bellows, compensator). The rear part carries the vertical tail area and aerodynamically finishing with the aircraft.
TTD:
length: 4.9 m
wingspan: 5,3 m
height: 1.2 m
wing area: 3 m2
takeoff weight without chassis: 110 kg
source:
L+K no. 19/1978, str. 78.
Towed target KT-04 was part of the training complex of aircraft L-39. Was vlekán aircraft L-39V. Target is all-metal with samonosným wing. Has SOP, VOP does not. The hull has three parts. In the front is zavěsné devices for connecting ropes, landing parachute, the mechanism of its opening, electric control system and battery. Under the middle part is composed of an inflatable bag for a cushion landing and two curtains for the ejection of the chassis. Inside is a pneumatic installation with a bottle of compressed air for inflating amortizátoru (buffer bellows, compensator). The rear part carries the vertical tail area and aerodynamically finishing with the aircraft.
TTD:
length: 4.9 m
wingspan: 5,3 m
height: 1.2 m
wing area: 3 m2
takeoff weight without chassis: 110 kg
source:
L+K no. 19/1978, str. 78.
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