Difference between revisions of "RE-L10 "Poodle" Liquid Fuel Engine"
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The primary intended role of this engine is for larger upper stages of rockets for orbital insertions, transfers, and landings. In the past, it has been outperformed in these by [[LV-T30 Liquid Fuel Engine]]s and clusters of [[LV-909 Liquid Fuel Engine]]s, though this is no longer the case. | The primary intended role of this engine is for larger upper stages of rockets for orbital insertions, transfers, and landings. In the past, it has been outperformed in these by [[LV-T30 Liquid Fuel Engine]]s and clusters of [[LV-909 Liquid Fuel Engine]]s, though this is no longer the case. | ||
| − | == | + | == Product description == |
| − | {{Quote|A more reasonable engine for rough economic times, the Poodle engine doubles as a BBQ when at low power. | + | {{Quote|A more reasonable engine for rough economic times, the Poodle engine doubles as a BBQ when at low power.}} |
== Changes == | == Changes == | ||
Revision as of 18:04, 4 August 2014
| RE-L10 "Poodle" Liquid Fuel Engine | ||
 | ||
| Liquid fuel engine by Rockomax Conglomerate | ||
| Radial size | Large | |
| Cost | (total) | 1 300.00 
|
| Mass | (total) | 1.750 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Heavy Rocketry
| |
| Unlock cost | 4 200
| |
| Since version | 0.16 | |
| Part configuration | liquidEnginePoodle_v2.cfg | |
| Maximum thrust | (1 atm) | 64.29 kN |
| (vacuum) | 250.00 kN | |
| Isp | (1 atm) | 90 s |
| (vacuum) | 350 s | |
| Fuel consumption | 14.57  /s
| |
| Thrust vectoring | 5 ° | |
| Electricity generated | 8.0 ⚡/s | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | Yes | |
| In an orbit | Yes | |
| On an escape | Yes | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
| Packed volume | None | |
The Rockomax "Poodle" Liquid Engine, formerly designated LV-909 Liquid Fuel Engine (Large), is a size 2 (2.5 meter diameter) liquid fuel engine. It has a moderate thrust to weight ratio, offset by its relatively short height, high Isp and thrust, and wide gimbal range.
The primary intended role of this engine is for larger upper stages of rockets for orbital insertions, transfers, and landings. In the past, it has been outperformed in these by LV-T30 Liquid Fuel Engines and clusters of LV-909 Liquid Fuel Engines, though this is no longer the case.
Product description
| “ | A more reasonable engine for rough economic times, the Poodle engine doubles as a BBQ when at low power. | ” |
Changes
- cost increased (600 → 1600), mass reduced (2.5 → 2)
- Retextured
- (Part rebalancing) Mass reduced from 4 to 2.5, thrust increased from 135 to 220.
- Initial release (with LV-909 title and description)
