User:Xingqiu Viator/sandbox: Difference between revisions
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== Xingqiu's personal sandbox dump == |
== Xingqiu's personal sandbox dump == |
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{{Infobox rocket|name=RFA One|country-origin=Germany|manufacturer=Rocket Factory Augsberg AG|cpl=ca. 3 million €|stages=3|height=30 meters|diameter=2 meters|LEO-payload=1,600 kg|status=In development|stage1engines=9x Helix|stage1thrust=~ 100 kN|stage1SI=325 s|stage1fuel=RP-1/LOX}} |
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Revision as of 12:49, 31 March 2023
Don't. Just. Don't interfere.
What the hell did I just do? Note that the 'Collei' and 'Kazuha' infobox are made for practice: sandbox open-mindedness is advised as the user hones its skills again for editing.
Practice infobox section for aircraft articles without any infobox
This is an example of an infobox.
| Model 3 'Collei' | |
|---|---|
| Role | Fighter |
| Manufacturer | Autumn Aircraft and Motor Company |
| First flight | 1934 |
| Introduction | 1935 |
| Developed from | XP-111.1 proposal |
The Autumn Aircraft and Motor Company 'Collei' (Model 3) is a fictional single-place monoplane that would have been powered by a R-1535 radial piston engine. It remained a paper project.
Infobox for Curtiss P-18 pursuit
The Curtiss XP-18 was ordered in 1930...
| Curtiss XP-18 | |
|---|---|
| Role | Fighter |
| National origin | United States |
| Manufacturer | Curtiss Aeroplane and Motor Company |
| First flight | Never flew |
| Introduction | 1930 (proposal) |
| Status | Cancelled |
| Number built | Never built |
Infobox for Curtiss P-19 pursuit
The Curtiss XP-19 was ordered in 1930...
| Curtiss XP-19 | |
|---|---|
| Role | Fighter |
| National origin | United States |
| Manufacturer | Curtiss Aeroplane and Motor Company |
| First flight | Never flew |
| Introduction | 1930 (proposal) |
| Status | Cancelled |
| Number built | Never built |
Signature Test
General Guhua Yukuaki • Chat with him • Long live the archons, long live Teyvat!
Xinghua (she/her) • Chat with her
• For use in April 1st.
Xingqiu's personal sandbox dump
meh
| Manufacturer | Rocket Factory Augsberg AG |
|---|---|
| Country of origin | Germany |
| Cost per launch | ca. 3 million € |
| Size | |
| Height | 30 meters |
| Diameter | 2 meters |
| Stages | 3 |
| Capacity | |
| Payload to LEO | 1,600 kg |
| Launch history | |
| Status | In development |
| First stage | |
| Engines | 9x Helix |
| Thrust | ~ 100 kN |
| Specific impulse | 325 s |
| Propellant | RP-1/LOX |