Editing Failing Witch:Volume2 Episode3 (section)

===Part 1===

Required Specs for the JX-401 SSTO Broom God: Version 3.51

User Name: <Anonymous>   Sent to: <Anonymous>



*This document is meant to succinctly share the valuable opinions of the relevant departments with the relevant universities and companies. You have already agreed to participate in this matter. We wish to rapidly complete a realistic plan that meets all the demands necessary to realize purely domestic space development infrastructure.



Crew: 1 (although more could fit in the cargo space)

Max Speed: Greater than Mach 9 (standard atmospheric flight), greater than Mach 30 (in vacuum and extra-atmospheric flight).

Max Altitude: More than 400km. Must be able to leave the atmosphere and enter low orbit unassisted.

Primary Propulsion System: JF-23 aviation fuel + oxygen ram jet engine x2 (standard atmospheric flight), X-5 liquid fuel + oxidant rocket engine (in vacuum and extra-atmospheric flight).

Primary Power Source: Large capacity lithium ion battery + storage alloy hydrogen oxygen fuel battery.

Max Continued Flight Without Resupply: more than an hour (standard atmospheric flight), 48 hours (in vacuum and extra-atmospheric flight using non-propulsion position stabilization).

Max Capacity: 25 tons (excluding fuel and oxidant).

Equipped Weaponry: None (for clearing debris, it is equipped with multipurpose joints x4 capable of instant attaching/detaching of chemical oxygen iodine laser, air-to-air missiles, Gatling gun, etc. But to remain in compliance with the Borderless Space Peace Treaty, avoid referring to these as ‘combat’ or ‘military’ weaponry).

Safety Level for Crew and Cargo: Level S as per global standard. Including the cargo space capable of carrying extra crew.

Procured Budget: 30 billion yen per craft. Do not exceed this under any circumstances.



(Hidden Note by Sending User: This again? The cargo space is too large for the size of the craft as a whole. I know this is unavoidable given our initial objective of constructing a purely domestic next-gen transport method that can open up the space development industry that has shut down since the collapse of the United States, but if we increase the inertial burden that far, we can’t fully eliminate the risk of it breaking apart mid-flight. Also, the manufacturing costs will change considerably depending on the markets for the different materials and how many are being manufactured! You imbeciles!!)