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VTOL Aviation India PVT. LTD. · India
Abhiyaan ENU800
VTOL Aviation India Abhiyaan ENU800
复合翼（升力＋巡航） · 阶段未核实 · 核查 2026-10-01
飞行构型与公司名称
复合翼（升力＋巡航）
VFS 原始目录分组：升力＋巡航。按目录所述推进方式归类。
核对构型依据 ↗原始目录分组：升力＋巡航
中文名称：待核实 · 原名：VTOL Aviation India PVT. LTD.
下列为 VFS 目录披露的参数，包含设计目标及历史版本信息。目录阶段不等于适航或量产状态；不同任务条件的航程与载荷不能直接当作同一条件下的性能。
资料覆盖与状态依据
可用性能指标 1/3 · 阶段未核实 · 目录依据 · 目录阶段，尚未核实批准状态
查看状态依据 ↗航程未纳入：单位或条件未能一致解析
巡航速度未纳入：单位或条件未能一致解析
订阅本机型报道 RSS →主要参数
- 座位／载员
- Cargo and/or combat equipment
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 航程（按来源口径）
- Unknown
- 巡航速度
- Unknown
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 200 kg (441 lb)
- 空重
- 未公开／未录入
- 长度
- 未公开／未录入
- 翼展
- 未公开／未录入
- 高度
- 未公开／未录入
- 动力来源
- Hybrid-electric with batteries or battery packs alone
- 电机
- 9 propellers
- 旋翼／螺旋桨
- 9 propellers
- 续航时间
- Unknown
- 飞行高度
- 未公开／未录入
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric or eVTOL heavy-lift military cargo/combat drone
- Piloting
- Autonomous
- Capacity
- Cargo and/or combat equipment
- Cruise speed
- Unknown
- Range
- Unknown
- Flight Time
- Unknown
- Top altitude
- 5,500 m (18,044 ft)
- Maximum payload
- 200 kg (441 lb)
- Propellers
- 9 propellers
- Electric Motors
- 9 propellers
- Power source
- Hybrid-electric with batteries or battery packs alone
- Fuselage
- Carbon fiber composite
- Wings
- 1 high wing
- Tail
- 1 t-tail
- Landing gear
- Tricycle fixed-wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.
明确提及本机型的报道
暂无明确匹配的公开报道；通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较，资料修改不等于实机性能发生变化。
暂无已保存的版本变化，后续目录刷新将保留快照。