Difference between revisions of "RT-10 "Hammer" Solid Fuel Booster/Box"
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m (BobBot moved page RT-10 Solid Fuel Booster/Box to RT-10 "Hammer" Solid Fuel Booster/Box: Renamed part after update.) |
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<noinclude>{{Data template used}}</noinclude> | <noinclude>{{Data template used}}</noinclude> | ||
{{Infobox/Part | {{Infobox/Part | ||
| − | |file=RT- | + | |file=RT-10_White.png |
|type=srb | |type=srb | ||
| − | |size= | + | |size=1 |
| − | | | + | |size2=r |
| − | |costs= | + | |costs=400 |
| − | |mass=0. | + | |mass=0.75 |
| − | |sf= | + | |sf=375 |
|drag=0.2-0.3 | |drag=0.2-0.3 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=7 | |tolerance=7 | ||
| − | |research= | + | |research=Basic Rocketry |
| − | |unlock cost= | + | |unlock cost=1200 |
|since=0.7.3 | |since=0.7.3 | ||
| − | |filename=solidBoosterRT- | + | |filename=solidBoosterRT-10_v2.cfg |
| − | |part= | + | |part=Size1_SRBs |
| + | |parent=Engine | ||
|more={{Infobox/Part/solid fuel engine | |more={{Infobox/Part/solid fuel engine | ||
| − | |thrust= | + | |thrust=227 |
| − | |isp-atm= | + | |isp-atm=170 |
| − | |isp-vac= | + | |isp-vac=195 |
| − | |fuel= | + | |fuel=375 |
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments= | + | |environments=60 |
| − | |staging= | + | |event=y |
| − | | | + | |staging=y |
| + | }} | ||
| + | {{Infobox/Part/tank | ||
| + | |sf=375 | ||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:27, 9 October 2024
| RT-10 "Hammer" Solid Fuel Booster | ||
 | ||
| Solid rocket booster by Found lying by the side of the road | ||
| Radial size | Small, Radial mounted | |
| Cost | (total) | 400.00 
|
| (dry) | 175.00
| |
| Mass | (total) | 3.563 t |
| (dry) | 0.750 t | |
| Drag | 0.2-0.3 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Basic Rocketry
| |
| Unlock cost | 1 200
| |
| Since version | 0.7.3 | |
| Part configuration | solidBoosterRT-10_v2.cfg | |
| Maximum thrust | (1 atm) | 197.90 kN |
| (vacuum) | 227.00 kN | |
| Isp | (1 atm) | 170 s |
| (vacuum) | 195 s | |
| Fuel consumption | 15.83  /s
| |
| Thrust vectoring | No | |
| Burn time | (1 atm) | 20.7 s |
| (vacuum) | 23.7 s | |
| Testing Environments | ||
| On the surface | No | |
| In the ocean | No | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | Yes | |
| In an orbit | Yes | |
| On an escape | No | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
| Solid fuel | 375
| |
