LV-T30 "Reliant" Liquid Fuel Engine/zh-cn
| LV-T30“信赖”液体燃料引擎 | ||
 | ||
| Liquid fuel engine 制造商： Jebediah Kerman废品回收和飞船部件公司 | ||
| 径向尺寸 | 小 | |
| 成本 | (总计) | 1 100.00 
|
| 质量 | (总计) | 1.250 吨 |
| 阻力 | 0.2 | |
| 最高承受温度 | 2000 开尔文 | |
| 最大冲击加速度 | 7 米/秒 | |
| 对应技术 |  通用火箭学
| |
| 解锁费用 | 3 200
| |
| 自版本 | 0.7.3 | |
| 部件配置文件 | liquidEngineLV-T30_v2.cfg | |
| 最大推力 | (1 标准大气压) | 205.16 千牛頓 |
| (vacuum) | 240.00 千牛頓 | |
| 比冲 | (1 标准大气压) | 265 秒 |
| (vacuum) | 310 秒 | |
| 燃料消耗量 | 15.79  /秒
| |
| 推力矢量 | 否 | |
| 发电量 | 7 ⚡/秒 | |
| 包裹容量 | 无 | |
LV-T30“信赖”液体燃料引擎是一个最基本的液体燃料引擎.
产品介绍
| “ | 尽管它被一些评论家们用一些微不足道的话比如“碎了一地”来批评，但LV-T系列发动机已证明其相对可靠。因为T30型号的故障率和粉碎率都低于50%，所以工程师和LV-T的支持者认为这相比于以前型号是一个重大进步。 — Jebediah Kerman废品回收和飞船部件公司 |
” |
Usage
As a liquid fuel engine, the Reliant has throttle control, shutdown and restart capabilities, making it easier to control vehicles safely and accurately. It also has nearly twice the specific impulse of the solid motors that went before it. It cannot be placed radially; however, since rocket fuel tanks can be placed radially, the Reliant can be the basis of liquid-fueled strap-on boosters in parallel configurations. Since the engine lacks thrust vector control, other means must be incorporated to make sure the vehicle remains pointed in the right direction, such as parts with reaction wheels, aerodynamic fins and control surfaces, and parallel operating gimbaled engines such as the LV-T45 "Swivel" Liquid Fuel Engine.
The Reliant has the highest Thrust to Cost ratio of any liquid fueled engine in the game, meaning it produces a kN of thrust most cheaply. This makes it one of the most cost-effective engines in career, although compensating for the lack of gimballing may cause the final rocket to be more expensive.
Trivia
- Previously, this engine was unlocked first in the tech tree, before the LV-T45 "Swivel" Liquid Fuel Engine. Its product number and description support the idea of the Swivel being a more advanced version of the Reliant.
- It is similar in appearance to the RS-56-OBA booster engine used by the late Atlas II rocket.
Changes
- Thrust increased from 215 to 240.
- Isp changed from 300 s vacuum/280 s at 1 atm to 310 s vacuum/265 s at 1 atm.
- Isp decreased from 370 s vacuum/320 s at 1 atm to 300 s vacuum/280 s at 1 atm.
- Cost increased from 850 to 1100 funds.
- Electricity production increased to 7.0
- Retextured and remeshed
- Alternator added, engine now gains 1.0 electricity
- Major CFG revision (most notably Isp added)
- (Bug fix) Liquid Engine particle effects responding to engine cutoff
- Initial release
