PDF《产品与服务》

产品与服务 朱雀一号(固体) ZQ-1 Three-staged Solid Propellant Engine Launcher 火箭级数:3 级The Stage of Rocket: Three stages 发动机推进组合:丁羟四组元 Engine Propulsion Combination: HTP-4 运载能力:200kg@500km SSO Payload capability:200kg@500km SSO 全箭总长:19 m Total Length:19m 箭体直径:1300mm Diameter:1300 mm 起飞质量:27t Lift-off Mass: 27t 起飞推力:45t Lift-off Thrust: 45t 朱雀二号(80T) ZQ-2 Two-staged LRE Launcher 优势:推进剂无毒无污染,甲烷燃料成本低廉,将来可拓展为可重复使用火箭 Advantage: Eco-friendly: low carbon emission, nontoxic, pollution-free, reusable 性能指标 Performance Index: 两级液体火箭 Two-staged Liquid Rocket 直径:3350mm Diameter: 3350mm 长度:48.

8m Total Length:48.8m 起飞重量:216 t Lift-off Mass: 216t 起飞推力:268t Lift-off Thrust: 268t 运载能力: 1800kg@500km SSO 1500kg@700km SSO 4000kg @200km LEO Launch Capacity: 1800kg@500km SSO 1500kg@700km SSO 4000kg @200km LEO 发射服务 我们基于ZQ-1/ZQ-2运载火箭提供发射服务综合解决方案 中小型运载火箭的研制 发射基地协调与运作 测控支持与协调 保险安排 Land Space will provide the systematic launch service solution based on ZQ-2 launcher 1. Small/medium launchers R&D 2. Launch site coordination & operations 3. TT&C support and coordination 4. Insurance placement ZQ-2用户接口 有效载荷包络(整流罩尺寸、有效容积、适配器设计策略等) 整流罩尺寸和有效载荷可用空间:见下图1: 载荷适配器设计策略:与所有主流S/C适配器兼容. 根据客户的要求,ZQ-2运载火箭使用国际标准适配器类型,如937B、1194/1194A和φ660mm夹带分离系统与卫星 接口,也可按照用户需求对其进行调整,以适应用户指定的卫星分离系统(如φ400mm).蓝箭航天提供适应于各种 非标准有效载荷接口的技术服务. Payload envelope (fairing dimensions, useful volume, adapter design policy, etc) Fairing dimensions and Useful volume: See Figure

2 below: Adapter design policy: Compatible with all main stream S/C adapters. Per customer request, ZQ-2 launch vehicle uses the international standard adapter types as 937B, 1194/1194A, and φ660mm clamp band separation system to interface with the satellites, which can be modified to accommodate satellite standard separation systems (e.g., φ400mm) as well. Requests for accommodation of any non-standard payload interface can also be accommodated through technical coordination with LANDSPACE. : Figure

1 ZQ-2 Payload Fairing ( With Cutaway) Table

4 ZQ-2 Main Technical Data of Payload Fairing ZQ-2 整流罩的主要参数 ZQ-2载荷入轨精度 ZQ-2可达到较高的入轨精度.具体的入轨精度取决于不同任务类型和有效载荷. 最低目标轨道入轨精度: -半长轴偏差:Δa≤5km -倾角偏差:Δi≤0.02 -偏心偏差:E≤0.002 Payload Injection Accuracy The design of ZQ-2 is aiming at repairing the trajectory deviation to achieve a high orbital injection accuracy. Injection accuracy will be mission dependent and reliant on the payload. LANDSPACE will ensure the following minimum target orbital insertion accuracy: - Semi-major Axis Deviation: |Δa|≤5km - Inclination Deviation: |Δi|≤0.02 - Eccentricity Deviation: e≤0.002 ZQ-2入轨分离姿态精度 ZQ-2提供一系列轨道部署方向选项,包括惯性、轨道相对和太阳指向.表3给出了典型的ZQ-2有效载荷预分离姿态角 精度和角速度精度. Typical Pre-Separation Attitude and Spin-Rate Accuracy The separation attitude is selected by the satellite mission planners to satisfy payload requirements. ZQ-2 provides a range of deployment direction options, including inertial, orbit-track-relative, and sun-pointing. Table