User:Vyacheslav84/ttrutyu
| г л | |
| Country of origin | рп |
|---|---|
| Date | прр |
| First flight | про |
| Last flight | рпорп |
| Designer | аппа |
| Manufacturer | апр |
| Application | роььб |
| Associated LV | полл |
| Predecessor | прр |
| Successor | пп |
| Status | прло |
| Liquid-fuel engine | |
| Propellant | пгоо / пра |
| Mixture ratio | авп |
| Cycle | ывпр |
| Pumps | авпрп |
| Configuration | |
| прап | |
| Chamber | прап |
| Nozzle ratio | апрап |
| Performance | |
| Thrust | птрпа |
| at altitude | апртап |
| Thrust, vacuum | аптрап |
| Thrust, sea-level | апртпа |
| Thrust-to-weight ratio | иптпт |
| Chamber pressure | прапт |
| Specific impulse | апртпа |
| Specific impulse, vacuum | аптр |
| Specific impulse, sea-level | партпао |
| Total impulse | авптрпа |
| Burn time | парпто |
| Propellant capacity | апрп |
| Dimensions | |
| Measurement | апорап |
| Length | апртоап |
| Diameter | автап |
| Dry weight | авпротпа |
| Used in | |
| аптоп | |
| References | |
| References | апротт |
| Notes | апт |
| File:1 1 | |
| Country of origin | 1 |
|---|---|
| Date | 1 |
| First flight | 1 |
| Last flight | 1 |
| Designer | 1 |
| Manufacturer | 1 |
| Application | 1 |
| Associated LV | 1 |
| Predecessor | 1 |
| Successor | 1 |
| Status | 1 |
| Solid-fuel motor | |
| Propellant | 1 / 1 |
| Grain | 1 |
| Core | 1 |
| Casing | 1 |
| Nozzle | 1 |
| Configuration | |
| 1 | |
| Chamber | 1 |
| Nozzle ratio | 1 |
| Performance | |
| Thrust | 1 |
| at altitude | 1 |
| Thrust, vacuum | 1 |
| Thrust, sea-level | 1 |
| Thrust-to-weight ratio | 1 |
| Chamber pressure | 1 |
| Specific impulse | 1 |
| Specific impulse, vacuum | 1 |
| Specific impulse, sea-level | 1 |
| Total impulse | 1 |
| Burn time | 1 |
| Propellant capacity | 1 |
| Dimensions | |
| Measurement | 1 |
| Length | 1 |
| Diameter | 1 |
| Dry weight | 1 |
| Used in | |
| 1 | |
| References | |
| References | 1 |
| Notes | 1 |
| File:1 1 | |
| Date | 1 |
|---|---|
| First flight | 1 |
| Last flight | 1 |
| Designer | 1 |
| Manufacturer | 1 |
| Application | 1 |
| Associated LV | 1 |
| Predecessor | 1 |
| Successor | 1 |
| Status | 1 |
| Hybrid engine | |
| Propellant | 1 / 1 |
| Configuration | |
| 1 | |
| Chamber | 1 |
| Nozzle ratio | 1 |
| Performance | |
| Thrust | 1 |
| at altitude | 1 |
| Thrust, vacuum | 1 |
| Thrust, sea-level | 1 |
| Thrust-to-weight ratio | 1 |
| Chamber pressure | 1 |
| Specific impulse | 1 |
| Specific impulse, vacuum | 1 |
| Specific impulse, sea-level | 1 |
| Total impulse | 1 |
| Burn time | 1 |
| Propellant capacity | 1 |
| Dimensions | |
| Measurement | 1 |
| Length | 1 |
| Diameter | 1 |
| Dry weight | 1 |
| Used in | |
| 1 | |
| References | |
| References | 1 |
| Notes | 1 |
| File:1 1 | |
| Date | 1 |
|---|---|
| First flight | 1 |
| Last flight | 1 |
| Designer | 1 |
| Manufacturer | 1 |
| Application | 1 |
| Associated LV | 1 |
| Predecessor | 1 |
| Successor | 1 |
| Status | 1 |
| 1 monopropellant | |
| Configuration | |
| 1 | |
| Chamber | 1 |
| Nozzle ratio | 1 |
| Performance | |
| Thrust | 1 |
| at altitude | 1 |
| Thrust, vacuum | 1 |
| Thrust, sea-level | 1 |
| Thrust-to-weight ratio | 1 |
| Chamber pressure | 1 |
| Specific impulse | 1 |
| Specific impulse, vacuum | 1 |
| Specific impulse, sea-level | 1 |
| Total impulse | 1 |
| Burn time | 1 |
| Propellant capacity | 1 |
| Dimensions | |
| Measurement | 1 |
| Length | 1 |
| Diameter | 1 |
| Dry weight | 1 |
| Used in | |
| 1ё | |
| References | |
| References | 1 |
| Notes | 1 |