Welcome to the Jupiter Spacecraft Technical Manual. This guide is your ultimate resource for understanding and mastering the features, systems, and operations of this versatile spacecraft. It covers every essential detail to help you navigate, maintain, and fully utilize the Jupiter Spacecraft to its maximum potential.




Pages Included in this manual:



- Systems
| Detailed explanation of onboard systems and their functionality.

- Antenna & Distress Beacon
| Guide to setting up communication systems and emergency signals.

- Fuel Consumption
| Information on fuel efficiency and consumption rates.

- Connecting & Refueling
| Guidelines for docking and refueling procedures.

- Max weight and Cargo capacity
| Specifications for cargo capacity and weight limitations.

- Thruster Efficiency / Maximum Recommended Gravity
| Performance data for thrusters under varying gravity conditions.

- Automated Systems
| Overview of automated features.

- Gas Storage & Production
| Details on fuel and oxygen storage, as well as their systems for renewal.

- Flight Seat Hotbars
| Explanation of the flight seat controls and hotbar assignments.

- Takeoff Sequence
| Step-by-step guide to ensure a smooth launch.

- Landing Sequence
| Procedures for safe and controlled landings.

- Oribtal Trajectory
| Tips for achieving an escape trajectory according to designed flight specifications.

- Garage / Chariot
| Description of the onboard garage and its vehicle, the Chariot.

- Chariot Specifications And Usage
| Details on the Chariot's design and operational guidelines.

- Engineering Access / Repair
| Instructions for accessing engineering systems and performing repairs.

- Emergency procedures
| Protocols for handling emergencies, including system lockouts and evacuations.

- Troubleshooting
| Solutions to common issues and system malfunctions.

- Terms of Use
| Information on the intended use and operational limitations.

- Credits
| Acknowledgments for contributors and sources.

The Jupiter Spacecraft is equipped with 141 gyroscopes to maintain its stability and orientation during flight. These gyroscopes are essential for counteracting any unwanted spin or rotation that may occur, ensuring smooth and precise maneuvers. The system is crucial for maintaining control in zero-gravity environments and during high-speed travel or complex navigation tasks.

Key Features:

• 141x Gyroscopes for stability and orientation control.
  
• Counteracts unwanted rotation, ensuring smooth and stable flight.
  
• Essential for precise navigation during delicate maneuvers.

The Jupiter spacecraft is equipped with an array of hydrogen thrusters that power both space travel and atmospheric operations. These include:

• 117x small hydrogen Thrusters
  
• 72x large hydrogen Thrusters
  
• 12x large retractable VTOL Thrusters

Theese are providing the spacecraft with versatile propulsion capabilities. The retractable VTOL engines allow for vertical take-off and landing, offering heightened maneuverability during planetary landings or take-offs. The remaining thrusters ensure the ship maintains precise control and stability during flight.

The Life Support system on the Jupiter Spacecraft is responsible for maintaining a safe and habitable environment for the crew. It regulates essential factors such as oxygen levels, temperature, humidity, and air quality, therefore ensuring that the crew can stay safe and comfortable during long missions in space or on planetary surfaces.

The Jupiter Spacecrafts Life Support Systems can support up to 12 People with the oxygen scrubbers, if the O2/H2 Generation system is offline the tanks can support a standard crew of: 5 for up to 353 Hours (Roughly 14.5 Days).

The Life Support [LS] System:

• 1x Survival Kit
  
• 4x O2/H2 Generators
  
• Temperature and Humidity Control
  
• Oxygen Regulation

The Jupiter Spacecraft is equipped with a highly advanced transmitter array, ensuring seamless communication across vast distances in space. The system is designed for long-range communication, allowing the crew to stay in contact with other ships, space stations, or ground-based command centers for a range up to 50km.

The Spacecraft is also equiped with a Distress Beacon of which can be activated in the terminal or a button up by the comms chair behind the pilot's seat.

The Jupiter Spacecraft is equipped with hydrogen turbines (H2 engines) that provide supplemental power for the spacecraft’s auxiliary systems. These turbines are designed to generate energy efficiently by converting hydrogen fuel into power, supporting both the propulsion system and secondary systems such as life support, navigation, and communication. The use of hydrogen ensures clean and environmentally friendly energy production by use of ice, reducing reliance on other fuel sources.

Key Features:

• Efficiently converts hydrogen into power for various spacecraft systems.
  
• Provides power for propulsion and auxiliary systems.
  
• Hydrogen fuel offers clean energy with minimal emissions.
  
• Offers a backup power source to ensure continuous operations even during high-demand situations.

The Jupiter Spacecraft is engineered for transport of personell and some cargo while maintaining safety and performance. Recognizing its weight limitations is essential for effective mission planning, particularly in varying gravity environments.



Unloaded Weight: The base weight of the Jupiter Spacecraft is 936,750 kg, inclusive of all core systems and fully loaded hydrogen tanks.

Cargo Capacity in Standard Gravity (1g)
Maximum Recommended Cargo: 80,000 kg.
With this cargo, the total spacecraft weight is 1,016,750 kg, ensuring optimal performance and safety during operations in standard gravity environments.
This is the maximum safe limit for extended operations in 1g.



Cargo Capacity in Higher Gravity (1.2g)
Maximum Cargo: In environments with higher gravity (up to 1.2g), the cargo capacity is reduced to 60,000 kg.
Total spacecraft weight with this cargo is 996,750 kg.
Limiting cargo in higher gravity prevents excessive strain on the propulsion system and structural components.



The Jupiter Spacecraft is not designed for sustained operations in gravitational environments exceeding 1.2g.
Exceeding this gravity threshold with heavy loads can compromise the integrity of key systems, including landing gear, structural supports, and thrusters.



Proper weight distribution is critical, especially with additional cargo.
The onboard system continuously monitors the total weight and gravity effects.



Impact of Overloading
Exceeding recommended cargo limits can:

• Drastically increase fuel consumption.
  
• Compromise thrust efficiency, resulting in sluggish flight and reduced maneuverability.
  
• Place excessive stress on landing gear during takeoff and landing sequences.

The spacecraft is equipped with a large, modular cargo bay optimized for secure storage.
Reinforced tie-down points and magnetic clamps prevent cargo shifts during flight.

The Jupiter Spacecraft features expansive gas and cargo storage systems, designed for both efficiency and safety. The gas storage compartments are built to handle hydrogen and oxygen required for the spacecraft's operations. The cargo hold; Often refered to as "The Garrage" provides ample space for the storage barrels filled with supplies, equipment, and materials needed for colonisation. However the larger storage system is accessable from the aft upper airlock.

The 8x O2 Tanks can store up to 400,000 L of Oxygen
And
The 23x H2 Tanks can store a total of 11,500,000 Liters of Hydrogen

Key Features:

• Dedicated compartments for storing hydrogen and oxygen.
  
• Spacious storage for supplies, scientific equipment, and mission essentials.
  
• Safely stores hazardous materials and sensitive items in separate compartments.
  
• The Terminal tracks stored items and provides real-time data on available resources.

The Jupiter Spacecraft is equipped with an advanced gas production system capable of generating hydrogen and oxygen from ice found in space or on planetary surfaces. This system ensures a continuous and Semi-self-sustaining supply of the gases needed for both fuel and breathable air. By harnessing local resources, the spacecraft, while dependent on refueling for efficient operation has the most high tech gas production system which reduces reliance on external refueling, therefore expanding its mission profile to allow for longer missions and greater autonomy.

The Jupiter Spacecraft has 4x O2/H2 Generators of which each produce:
100 L/s of Hydrogen
and
50L/s of Oxygen,

therefore the ship has a total output per second of:
400L/s of Hydrogen
and
200L/s of Oxygen.

The Jupiter Spacecraft is equipped with a quad leg landing gear system, designed for safe and stable landings on a variety of planetary surfaces. The system features retractable landing struts that are capable of absorbing shock upon touchdown (7.5M above ground is MAX recommended distance), ensuring that the spacecraft remains intact and undamaged during atmospheric entry or landing. Additionally, the landing gear system is built for durability, capable of withstanding the harsh conditions of both planetary surfaces and the vacuum of space.

The Jupiter Spacecraft is equipped with an advanced automated emergency evacuation system, designed to ensure the safety of the crew in case of critical failure or impending danger. This system triggers a series of predefined protocols to evacuate the crew quickly and efficiently, while minimizing the risk of injury or loss of life. The system includes automated alerts, evacuation route guidance leading the crew to the EVA airlock and safest exit away from the flight direction of the vehicle.

Key Features:

• In the event of low power the ship will ground itself therefore stopping any ability to take off, unless the batteries are recharged the jupiter can only be flown by pressing the override button next to the pilot's seat.
  
• If the fuel level goes below 15% the low fuel warning goes on, this enables blinking emergency lights throughout the ship.
  
• In the event of the hydrogen tanks being empty and the power being below 5%, the ship wont be able to spool the turbines to generate new energy. This situation causes the ship to initiate evac procedures initiating stationary red emergency lights, and the circular orange evac pattern lights to lead the way to the aft EVA airlock.

The Takeoff Procedure is relatively simple to those of which are trained to fly a Jupiter spacecraft

To initiate the takeoff under normal flight conditions do as the following:

1. Extend the VTOL Engines [Hotbar 1 , Button 2]

2. Initiate the main Engines [Hotbar 1, Button 1]

3. After engines are extended you can release the landing gear [Hotbar 1, Button 8]

4. After the landing gear has unlocked from the surface, you can initiate takeoff vertically.

5. After having taken off to about 100 meters, Raise the landing gear by pressing
[Hotbar 1, Button 6] and keep thrusting up but start thrusting forward and pitch up 30° On the vertical axis.

6. After having pitched up 30°, keep thrusting forwards and release the upwards thrust (spacebar) after releasing the upwards thrust you should retract the vtol engines:
[Hotbar 1, Button 2]

7. After having reached the desired altitude of which is most commonly 500m you can re-align the ships vertical axis to match the horizon, And press [Hotbar 1, Button 4] to set forward engines to override at 4% and save fuel. In the case of slowing down press [Hotbar 1, Button 5] until your engine's overrides are back in manual control: 0%

That concludes the Take-Off Procedure.





The Landing Procedure alike the takeoff sequence is relatively simple to complete but requires a bit more delicacy when flying.

To initiate the Landing Procedure under normal flight conditions do as the following:

1. Approach the desired landing area and flatten out your flight axis to match the horizon (Ensure thruster overrides are at 0% [Hotbar 1, Button 4 & 5]),

2. continue to gradually drop the ship down to an altitude of 80m and extend the VTOL Engines
[Hotbar 1, Button 2]

3. After engines are extended you can extend the landing gear [Hotbar 1, Button 6]

4. After the landing gear has been extended you can continue to slowly approach the desired landing area.

5. After having approached the ladning area with rougly 30m of altitude you can either tap "C" to go down or a more stable and slow descent, tapping on and off the dampeners using "Z". Do this until you touch town onto the ground in which case you follow the next step.

6. After having landed, lock your landing gear using
[Hotbar 1, Button 7]
and retract your VTOL engines,
[Hotbar 1, Button 2]
after which you will de-activate your main engines:
[Hotbar 1, Button 1]

7. After having done so, your ship has now landed and you have secured the ship in its landing position.

That concludes the Landing Procedure.




The Orbital Trajectory is a continuation after the Take-Off Sequence, in which you do the following:

Instead of continuing to point 7 in the Take-Off Sequence, Do as following:

1. Pitch up to 80° and increase thrust override to ensure a stable max speed without loosing altitude, its is recommended to increase the thrust override before pitching up to 80°.

2. After 80° pitch has been reached, ensure that the thrust override is at the minimu required to stay at maximum velocity. As you are staying at the max speed, reduce the override as the planetary gravity is going down to ensure that you save all the fuel you can during Orbital Flight.

3. When you have reached orbit you are complete with the Orbital Trajectory Sequence.

The Jupiter Spacecraft includes a multi-functional garage designed to facilitate planetary colonization and exploration readiness. The garage serves as a secure storage area for mission-critical supplies, equipment, and the Chariot. It also provides the necessary resources and tools to construct essential structures for initial colonization efforts.


The garage is stocked with components and materials to assist in setting up a basic operational base, including:

• 8x Backup Canvases for parachute deployment.
  
• 1,000 Platinum Ingots for advanced component production.
  
• 1,000 Uranium Ingots for future energy needs.

Components to build:
• 30x Large Light Armor Blocks.
  
• 1x Prototech Refinery (Small Grid).
  
• 1x Large Grid Assembler.
  
• 1x Large Grid Battery.
  
• 2x Wind Turbines.
  
• 1x Large Grid Large Cargo Container.

• Secure Storage: Designed to protect supplies and the Chariot during transit and atmospheric entry.
  
  
• Deployment Assistance: Equipped with tools and systems to facilitate efficient unloading and assembly of colonization components.

The Chariot is a highly adaptable all-terrain vehicle designed for exploration and transport on planetary surfaces. Its rugged design makes it an essential tool for conducting surveys, transporting personell, and supporting colonization efforts.

The Chariot is powered by an array of high-capacitance small power-cells of which stores a total of 600kWh allowing for an opertional duration of up to 3 Hours of driving or 24+ hours of stationary keeping before needing to be recharged at a port or in the Jupiter's docking mount in the garrage.

The chariot can be launched by pressing:
[Hotbar 1 Button 5] to toggle the power supply to Auto, followed by
[Hotbar 1 Button 4] to unlock from the docking station its connected to, followed by driving out of said area / garrage.

The side doors for passengers can be opened in the Chariot's cockpit by pressing buttons [1 & 2] on [Hotbar 1] to toggle each door separately.

The Chariot's Spotlights can be toggled on [Hotbar 1, Button 3]

To enable Winter Mode:

Raise the wheels power and friction by using buttons:
[6 & 8 on Hotbar 1] and increase both to 100%
To disable Winter Mode return both settings to each of their seperate values by using buttons:
[7 & 9 on Hotbar 1]
Original value of Power: [25%]
Original value of Friction: [50%]

After Re-Docking:
Set the batteries to recharge [Hotbar 1, Button 5] to ensure 100% charge for the next adventure!

If the Chariot is struggling to move down with the terrain due to the gyros, you can disable the override gyro on [Hotbar 2, Button 2]

• All-Terrain Capability: Optimized for travel over various surfaces, including rocky, sandy, and icy terrain.
  
• Durability: Engineered to withstand extreme planetary conditions and prolonged use.
  
• Modularity: Easily modified to meet mission-specific requirements, such as adding a fuel or cargo trailer for additional transport capabilities.

The Jupiter Spacecraft is designed with both autonomy and ease of use in mind, but there will be times when you need to connect to external sources for fuel, power, or other essential resources. This section outlines the procedures for docking and refueling, which are crucial for long-duration missions or when in remote locations where resources are limited.

Connecting to Docking Ports

Info: Docking Ports are located in the aft or hidden under plates in the back by the garrage ramp.

Approach the Docking Station:

• Ensure that the docking port is aligned and within range of the spacecraft’s docking system.
  
• Approach slowly using low thruster power to prevent any damage to the ports.
  
• Dock to the selected connector by using the correct hotbar button that can be found in the Hotbars section of this manual.

Activate Docking Procedures:
Once securely docked, access the correct hotbar and enable Stockpile of both O2 and H2 if external source is avalable, If external sources arent avalable: DO NOT ENABLE STOCKPILE; This will then disable the source of H2 for the thrusters or oxygen for the life support.

As a large vessel, the Jupiter Spacecraft requires a substantial amount of fuel to operate efficiently across vast distances. This fuel is primarily stored and used in the form of gaseous hydrogen, which powers the spacecraft’s thrusters and turbines. Due to its size and complexity, fuel management is a key consideration for long-term missions, requiring precise calculations and careful monitoring to ensure operational continuity. In this section, we will explore the spacecraft’s fuel consumption rates, its storage systems, and the strategies used to optimize fuel efficiency throughout your journey.

Fuel consumption for the Jupiter Spacecraft is directly influenced by its size, weight, and the complexity of its systems. Due to the extensive use of hydrogen as fuel, understanding how the spacecraft consumes this resource is crucial for mission planning and execution.

The Hydrogen Thrusters, which provide propulsion for the vessel, are one of the largest consumers of fuel. Their consumption is determined by the total thrust required to maintain the spacecraft's velocity, as well as adjustments made for orbital corrections and trajectory changes. The Retractable VTOL Engines, while used mainly for vertical takeoff and landing, also contribute to fuel usage, particularly in atmospheric or gravitationally intensive environments.

Given the large storage capacity of the spacecraft, it is essential to balance fuel consumption with available storage. This balance is monitored continuously, and the fuel consumption rate is adjusted according to the spacecraft's current operational status. Fuel efficiency can be optimized through careful management of the vessel's energy output and thrust requirements, which minimizes fuel waste and ensures that the Jupiter Spacecraft can sustain long-term missions.


As a large spacecraft, the Jupiter Spacecraft requires substantial thrust to maintain flight and accommodate varying cargo loads. Below is a detailed breakdown of the thrust calculations, factoring in both standard weight and heavy cargo, along with the resulting flight times under different throttle settings.

Standard Weight and Thrust Requirement
The Jupiter Spacecraft, when fully loaded with its standard weight of 936,750 kg, requires a total thrust of 9,544.8 kN to stay airborne. The spacecraft is equipped with the following thrusters:

67 Small Upwards Thrusters, producing 6,580.8 kN of thrust
10 Large Upwards Thrusters, producing 4,800 kN of thrust
This results in a total available thrust of 11,380.8 kN.

With this thrust output, the spacecraft can easily maintain flight, leaving a surplus of 1,836.0 kN for maneuvering, cargo management, or other operations.

When additional cargo is added, the spacecraft needs more thrust to maintain flight. For example, adding 80,000 kg of cargo requires an additional 864 kN of thrust.

After accounting for the extra load, the remaining thrust available would be:

Total thrust: 11,380.8 kN
Required thrust for standard weight: 9,544.8 kN
Required thrust for added cargo: 864 kN
This leaves 972.2 kN remaining, which is sufficient to manage the additional weight. The spacecraft can still operate with the increased load, but its flight will be slower and less responsive than with the standard weight.

Flight Time Estimates
The flight time of the Jupiter Spacecraft is heavily influenced by the amount of thrust applied and the resulting fuel consumption. With standard cargo weight (936,750 kg), the spacecraft can sustain flight for approximately 40 minutes with the minimum thrust required for hovering in 1g of gravity.

Throttle Overrides:
4% Override (Forwards Thrust)

When a 4% override forward throttle is applied, the flight time decreases slightly to 39 minutes. This is due to the increased fuel consumption caused by the additional forward thrust, but it allows for faster travel.

Full Throttle (Forwards Thrust)

At full throttle, the flight time is significantly reduced to 14 minutes. This sharp decrease reflects the heavy fuel consumption at maximum forward thrust.

Full Upwards Thrust

With full upwards thrust, the spacecraft can stay airborne for about 30 minutes, balancing the upward force required to maintain altitude and the fuel consumption rate.

It is crucial to utilize the 4% thrust override as outlined in the flight procedures. This slight adjustment significantly improves the spacecraft’s flight efficiency and extends flight duration. Failing to follow this procedure may lead to reduced operational time and could strain the system, potentially compromising the vessel's safety. Adhering to the documented thrust settings ensures optimal performance and security during extended missions.

The Jupiter Spacecraft is equipped with flight seat hotbars that provide quick access to essential systems and controls during operation. Understanding and recognizing the layout of these hotbars is crucial for efficient and safe flight. The hotbars are designed to give the pilot immediate control over key functions, from adjusting thrust levels to activating emergency systems. Familiarity with these controls ensures the crew can respond promptly in dynamic situations, making it an integral part of operating the vessel effectively.

The Jupiter Has 5 Hotbars:

Hotbar 1:

Slots:
1. Main Thrusters
2. Retractable Vtol Engines
3. Antenna
4. Thrust Override +
5. Thrust Override -
6. Toggle Retract/Extend Landing Gear
7. Lock Landing Gears
8. Unlock Landing Gears
9. Toggle O2/H2 Generators

Hotbar 2:

1. Toggle Aft Airlock Lights
2. Toggle Interior Lights
3. Toggle Circular Hallway Lights
4. Toggle Garrage Lights
5. Toggle Exterior Lights
6. Toggle Spotlights
7. Toggle Gyroscopes
8. None
9. Toggle Hydrogen Turbines [Backup Power]

Hotbar 3:

1. Toggle Survival Kit
2. Toggle Distress Beacon
3. Lock Hidden Underside Connectors
4. UnLock Hidden Underside Connectors
5. Toggle Stockpile H2 Tanks
6. Toggle Stockpile O2 Tanks
7. Toggle Recharge Jupiter Capacitor Cells
8. None
9. Toggle O2/H2 Generators

Hotbar 4:

1. Lock Aft Connectors
2. Unlock Aft Connecftors
3. Toggle Extend Vtol Engines
4. Toggle Main Thrusters
5. Toggle Switch Bottom Connectors
6. Toggle Hydrogen Turbines [Backup Power]
7. Toggle Chutes On/Off
8. Toggle Deploy Chutes
9. Toggle Auto-Deploy

Hotbar 5:

1. Toggle Lock Landing Gears
2. Toggle Manual Gear Door Plates
3. Toggle Manual Gear Inner Hinges
4. Toggle Manual Gear Outer Hinges
5. Toggle Manual Gear Pistons
6. None
7. None
8. None
9. None

Understanding how to access and maintain the Jupiter Spacecraft’s engineering systems is essential for ensuring long-term operational success. This section provides guidelines on how to perform basic repairs, troubleshoot common issues, and access key components of the spacecraft’s engine and structural systems. Regular maintenance is vital to prevent malfunctions and keep the spacecraft functioning at optimal performance.

The engineering access and repair room, located in the front starboard section next to the bridge entrance, serves as a critical hub for maintaining the Jupiter Spacecraft. From here, crew members can access vital systems, including the cargo hold, as well as the backrooms that house the thrusters and other essential systems. The layout is designed for quick access to the spacecraft’s primary functions, ensuring that any necessary repairs or maintenance can be conducted efficiently. This proximity to key areas of the spacecraft ensures that the crew can address issues with minimal delay, optimizing operational readiness and safety.

if components are damaged you can enter through:
Engineering-Hub -> Systems access door -> The Damaged System
However:
The VTOL-Engines can only be serviced from the exterior when extended.

This section provides solutions to common issues and malfunctions you may encounter while operating the Jupiter Spacecraft. It is essential to identify and address problems as they arise to ensure continued safe and efficient operations. Please follow the steps outlined below to diagnose and resolve potential issues. If the issue persists after following the troubleshooting steps, it is advised to contact qualified personnel for further assistance.



Symptoms: No power in capacitors or systems, unable to activate flight systems or navigate.

Possible Causes: Insufficient H2 fuel, malfunctioning batteries, or power is disabled.

Solution: Check fuel levels and ensure sufficient power is being supplied by batteries. If batteries are low, initiate charging protocols or replace them.


Symptoms: Unresponsive thrusters, reduced thrust output, or erratic behavior.

Possible Causes: Damaged thrusters, lack of fuel, or weight surpassed maximum recommended.

Solution: Inspect thruster components for damage, and check the fuel system level. Ensure no broken connections or external damage that might hinder functionality.


Symptoms: Unable to transmit or receive signals, or no communication between Remote-Controlled Grids.

Possible Causes: Damaged antenna array, lack of power.

Solution: Check antenna for damage and ensure the antenna is functioning properly. Reset the communication system distance or attempt a distance increase.


Symptoms: Low or fluctuating hydrogen supply, inability to generate power from turbines.

Possible Causes: Hydrogen tank leakage, little or no fuel remaining, or damaged storage systems.

Solution: Inspect hydrogen tanks for leaks or damage. Ensure the fuel supply is connected and functioning. Replace or repair damaged components as needed.


Symptoms: Evacuation system does not engage or guide crew to safety.

Possible Causes: Faulty Event Controllers, Timer failure, or manual lights override interruption.

Solution: Verify event controllers and timer system is working. Ensure power is supplied to the emergency systems.

• Always follow the standard procedures outlined in the emergency and operational manuals.
  
• Keep your systems up to date according to the workshop and periodically run diagnostic checks to ensure the spacecraft operates at peak efficiency.
  
• For technical assistance or unresolved issues, refer to the workshop comments or contact the creator: - Blank -.

By operating the Jupiter Spacecraft, the user agrees to adhere to the following terms and conditions:

• Intended Purpose: The Jupiter Spacecraft is designed for colonisation and space travel, including interplanetary missions, personell transport, and colonization support. While up to the user, it should only be used for these intended purposes or similar activities that align with its design.
  
  
• Operational Limitations: The spacecraft’s systems are designed to operate within specific parameters (e.g., fuel capacity, weight limits, thruster output). Users should ensure that the spacecraft is operated within these limits to avoid system malfunctions and to ensure safe operation.
  
  
• Safety Protocols: The spacecraft is equipped with automated safety systems, but operators must be familiar with all emergency procedures, including evacuation protocols and manual overrides. Negligence in adhering to safety procedures may result in malfunctions or accidents.
  
  
• Maintenance and Repair: The spacecraft must be regularly maintained to ensure optimal performance. The user is responsible for keeping the spacecraft’s systems in good working condition. Unauthorized modifications or failure to properly maintain the vessel could void warranties and migh lead to Clang or Malfunction.
  
  
• Fuel and Resources: The spacecraft uses hydrogen as its primary fuel source, which should be replenished periodically. Users are responsible for ensuring that the spacecraft is adequately fueled for its missions. Running out of fuel during flight may result in catastrophic failure or a crash.
  
  
• Liability: The manufacturers and developers of the Jupiter Spacecraft are not liable for damages resulting from misuse, accidents, or failure to follow operational procedures. The user assumes all responsibility for the safe operation of the spacecraft.
  
  
• Modification Restrictions: Any changes made to the design or functionality of the spacecraft and thereafter republishing shall not be done without the approval from the spacecraft’s engineers.
  
  
• Termination of Use: The right to operate the Jupiter Spacecraft is given to each user and can be frowned upon if the user fails to comply with these terms.
  
  
• Changes to Terms: The terms of use may be updated or revised periodically. The user is responsible for staying informed of any changes and agreeing to the updated terms.

NOTE: This section is sort of a joke, and some users might take this as a serious "Terms Of Use", it is purely made for fun and to help each user operate this vehicle successfully.

This technical manual was created to provide a comprehensive overview of the Jupiter Spacecraft, its systems, and operational guidelines. The following individuals and resources contributed to the design, engineering, and development of the spacecraft:

Building Team:

• Lead Builder: - Blank -
  
• Assistant Builder: Zeo
  
• Contributing Builder: TaliaT7

Contributors:

• Special thanks to Zeo for assistance with Building and teaching me how to build efficiently and well.
  
• LeoDraconus for input on the spacecraft's looks and "Emotional Support"
  
• TaliaT7 for providing insight into the accuracy and giving the spacecraft a pressurized garrage.

Acknowledgments:

• Special acknowledgment to The Oasis Community (Steam) (Discord)[discord.com] for their insights and support.
  
• The project has benefited from the community knowledge and open-source contributions from the Oasis[discord.com] community.