NASA · USA
RAVEN
NASA RAVEN
倾转旋翼 · 概念设计 · 核查 2026-10-02
飞行构型与公司名称
倾转旋翼
Propellers: 6 propellers (4 tilt-propellers and 2 VTOL-only stationary propellers). 2 tilt-propellers are mounted on wing tips. Two booms mounted under the high main wing, about 1/3 distance from the fuselage, have tilt-propellers at the front of the booms and stationary VTOL-only propellers on the
核对构型依据 ↗原始目录分组：矢量推力
中文名称：待核实 · 原名：NASA
每项参数附独立出处。厂商声明、目录转述与监管使用限制分别标明；设计目标和历史版本不等于当前实测性能。不同任务条件的航程与载荷请查看引用原文。
资料覆盖与状态依据
可用性能指标 0/3 · 概念设计 · 目录依据 · 目录阶段，尚未核实批准状态
查看状态依据 ↗巡航速度未纳入：单位或条件未能一致解析
概念参数，尚不代表已实现性能
订阅本机型报道 RSS →主要参数与逐项引用
- 座位／载员
- No pilot, no passengers[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Capacity: No pilot, no passengers
- 乘客
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 驾驶方式
- Remote piloting[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Piloting: Remote piloting
- 航程（按来源口径）
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 巡航速度
- Unknown[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Cruise speed: Unknown
- 最大速度
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 最大起飞重量
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 载荷
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 空重
- 1,000 lb (454 kg)[1] 来源 ↗
目录转述 · 设计目标／声明参数
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Empty weight (estimated): 1,000 lb (454 kg)
- 长度
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 翼展
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 宽度
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 高度
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 动力来源
- Batteries[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Power source: Batteries
- 电机
- 6 propellers[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Electric motors: 6 propellers
- 旋翼／螺旋桨
- 6 propellers (4 tilt-propellers and 2 VTOL-only stationary propellers). 2 tilt-propellers are mounted on wing tips. Two booms mounted under the high main wing, about 1/3 distance from the fuselage, have tilt-propellers at the front of the booms and stationary VTOL-only propellers on the rear of the booms.[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Propellers: 6 propellers (4 tilt-propellers and 2 VTOL-only stationary propellers). 2 tilt-propellers are mounted on wing tips. Two booms mounted under the high main wing, about 1/3 distance from the fuselage, have tilt-propellers at the front of the booms and stationary VTOL-only propellers on the rear of the booms.
- 续航时间
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 飞行高度
- Unknown[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Cruise altitude: Unknown
- 安全设计
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. In case of an emergency, the aircraft can land conventionally, with or without power, if there is a runway or unobstructed road available.[1] 来源 ↗
目录转述
依据与条件
Specifications:；目录转述，尚未用一手资料独立复核。
VFS World eVTOL Aircraft Directory · 核查 2026-10-02 · 来源未注明日期
Safety features: Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. In case of an emergency, the aircraft can land conventionally, with or without power, if there is a runway or unobstructed road available.
- 电池容量
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 充电时间
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 货舱容积
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 噪声
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
- 旋翼直径
- 未公开／待核实
未公开／待核实
依据与条件
未找到可引用的公开参数，不估算。
全部原始参数
Specifications:
- Aircraft type
- RAVEN uncrewed eVTOL technology demonstrator concept design aircraft[1] 来源 ↗
- Piloting
- Remote piloting[1] 来源 ↗
- Capacity
- No pilot, no passengers[1] 来源 ↗
- Cruise speed
- Unknown[1] 来源 ↗
- Hover flight time (expected)
- 10 minutes with a 25% battery reserve[1] 来源 ↗
- Cruise altitude
- Unknown[1] 来源 ↗
- Empty weight (estimated)
- 1,000 lb (454 kg)[1] 来源 ↗
- Propellers
- 6 propellers (4 tilt-propellers and 2 VTOL-only stationary propellers). 2 tilt-propellers are mounted on wing tips. Two booms mounted under the high main wing, about 1/3 distance from the fuselage, have tilt-propellers at the front of the booms and stationary VTOL-only propellers on the rear of the booms.[1] 来源 ↗
- Electric motors
- 6 propellers[1] 来源 ↗
- Power source
- Batteries[1] 来源 ↗
- Fuselage
- Carbon fiber composite[1] 来源 ↗
- Windows
- Panoramic wrap around windows[1] 来源 ↗
- Wings
- 1 main high wing[1] 来源 ↗
- Tail
- 1 conventional tail, with 1 vertical stabilizer and 1 horizontal stabilizer[1] 来源 ↗
- Landing gear
- Fixed tricycle wheeled landing gear[1] 来源 ↗
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. In case of an emergency, the aircraft can land conventionally, with or without power, if there is a runway or unobstructed road available.[1] 来源 ↗
补充检索来源
已检索 2026-10-02。下列为候选资料，尚未全部核实；参数依据请查看逐项引用，目录转述不等于厂商独立复核。
Raven | Size & Facts | Britannica ↗Raven vs Crow - What's the Difference and How to Tell Them Apart ↗RAVEN中文 (简体)翻译：剑桥词典 - Cambridge Dictionary ↗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。