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Technical Briefs:
The Time Shuttle Transportation System
(TTS)
Select Briefing
Mission Profile
Arcade 2084 isn't a time capsule. It's not simply a room of old games.
It's a "third place."
The sickness in our time: the collapse of public trust and the decline of civil discourse. The places where people used to meet are empty, gone, or poisoned. People retreat to their digital foxholes.
Vera's mission isn't to save video games. It's to save the idea of the arcade. A place you go to be with other people. A place with its own rules, its own culture, its own shared purpose. It's a physical space in a world that's gone virtual, a civil space in a world that's gone tribal.
The mission is rebuilding the social contract incrementally - starting on a small scale.
That's how the gap between us is closed.
Defender System Overview & Launch
The Time Shuttle, designation TTS-01 "Defender", represents the pinnacle of temporal transportation technology. Built in 2083, commissioned for a 2084 exhibition mission, it combines advanced Tachyon-8 particle manipulation with state-of-the-art navigation systems.
Exhibition Launch System: The Time Shuttle is launched first using a supplementary fuel tank with twin Solid Rocket Boosters (SRBs), similar to the original STS Orbiter launches.
Boosters and auxiliary fuel tank are jettisoned at altitude.
At approximately T+123 seconds and an altitude of 46,000 meters (150,000 ft), pyrotechnic fasteners release the SRBs.
SRBs reach an apogee of 67,000 meters (220,000 ft) before parachuting into the Atlantic Ocean.
The Time Shuttle continues using its main engines (TRS-25) in a heads-down orientation.
Flight & Temporal Operations
Descent & Time Barrier Penetration: At apogee, the TRS-25 engines ignite for a descent. When terminal velocity is reached (approximately 765 knots), the Tachyon drive propels the vehicle across the time barrier. The Time Shuttle then lands conventionally, remaining invisible to sensing technology developed prior to the 2060s.
Return Journey (See Launch Profile): The Time Shuttle uses remaining liquid fuel to launch from ground level, achieve transonic speed on ascent, and at 765 knots (880 MPH), the pilot engages the Tachyon drive to time-warp back to the future.
Temporal Navigation Rate: The Tachyon drive enables navigation through the continuum at a rate of 25 years per hour.
Physical Specifications & Cargo
Total Weight: Approximately 90 metric tons
Cargo Bay Dimensions: 20 meters long, ~5 meters diameter
Standard Cargo Capacity: Equivalent of fifty arcade machines (approx. 6.8 metric tons)
Maximum Payload: 50 metric tons
Weight and other specifics on equipment and fuel for the Tachyon drive are classified, but are thought to require the additional cargo capacity.
Core Systems
Temporal Core: Mallet Compensation Waveform Generator
Power Source: Tachyon-8 Particle Chamber
Navigation: Quantum-Aligned Temporal GPS
Life Support: Advanced Environmental Control System
Hull: Temporal Displacement Resistant Alloy
Safety Systems
Temporal Shielding: Prevents paradox exposure
Emergency Return Protocol: Automatic return to origin point
Quantum Stabilizers: Maintains temporal coherence
Paradox Detection Array: Early warning system
Mission Parameters
Primary Mission: Temporal preservation of historical artifacts (e.g., identifying and absconding with the best arcade machines of the 80s).
Secondary Objectives: Timeline observation and paradox prevention.
Maximum Temporal Displacement: 100 years.
Crew Capacity: 1 pilot, 2 passengers.
U.S. TEMPORAL AGENCY // TECHNICAL BRIEFING
TIME SHUTTLE DEFENDER (TTS-01) - UPDATED SPECIFICATIONS
//CLASSIFICATION: LEVEL 4 CHRONO-SECRET//EYES ONLY// //DOCUMENT ID: USTA-TS-2084-DEFENDER-SPEC-V2.1// //LAST REVISED: 04.05.2084//
OVERVIEW: The Time Shuttle Defender (TTS-01) is the first and only operational single-stage-to-orbit (SSTO) temporal insertion vehicle. Commissioned in 2083, its primary mission profile is autonomous operation in any historical time period without reliance on external launch infrastructure or refueling assets. The Defender is a self-contained system designed for high-performance atmospheric flight, orbital ascent, interplanetary transit, and controlled temporal displacement.
PROPULSION SYSTEM: TRS-25 FUSION DRIVE The heart of the Defender is its proprietary Tri-Reactant System 25 (TRS-25), a revolutionary compact fusion drive.
Type: High-Thrust Combined-Cycle Fusion Engine (x3)
Propellant: Cryogenic Deuterium/Helium-3 mix.
Reaction: Aneutronic D-He³ fusion, catalyzed by a high-energy Tachyon-8 (T8) particle injection matrix. This provides the immense energy density required for SSTO flight and temporal crossover initiation.
Sea-Level Thrust (per engine): 73,000 lbf (325 kN)
Total Sea-Level Thrust:219,000 lbf (974 kN)
Vacuum Thrust (per engine):95,000 lbf (423 kN)
Total Vacuum Thrust:285,000 lbf (1.27 MN)
Specific Impulse (Isp):
Air-Breathing(Ramjet) Mode: ~5,000 s
Rocket (Space)Mode: ~12,000 s
Mass Flow Rate: 535.5 kg/s (at full power)
PERFORMANCE METRICS
Launch Configuration Mass:150,081 kg (330,800 lbs)
Dry Mass (Structure & Systems): 69,000 kg
Onboard Propellant (Standard Load): 4,000 kg
Maximum Mission Payload: 50,000 kg (50 metric tons)
Thrust-to-Weight Ratio (at launch): 1.48
Ascent Profile: The Defenderis capable of a vertical SSTO ascent to a 100 km (Kármán line) apogee in 58 secondsunder full power.
Atmospheric Flight: Capable of conventional takeoff and landing on a 5,000-8,000 ft runway. Maximum atmospheric velocity is Mach 3+.
Temporal Crossover: Initiated by the TRS-25 drive, using the T8 Mallet Compensation Waveform to achieve safe, controlled transit through the time stream. Requires a full propellant charge for a standard 100-year jump.
TEMPORAL SYSTEMS
Tachyon-8 (T8) Containment Field: A multi-stage magnetic containment system that stores and regulates the T8 particles necessary for waveform generation and temporal shielding. The field is critical for protecting the vessel and its occupants from the corrosive effects of the time stream.
Chrono-Navigational Computer: A quantum-entangled processing core that calculates Mallet Waveform trajectories, accounting for gravitational variance and temporal drift. It is the only system capable of plotting a safe course through the time stream.
Temporal Displacement Sensor: Passive and active sensors that detect Mallet Waveform signatures, allowing the crew to identify other temporal events and vessels.
MISSION SYSTEMS
Matter Digitizer: A handheld or ship-mounted device capable of deconstructing inanimate matter into a stable data stream for storage and reconstruction. Primary use is for mission payload acquisition and cargo management.
Inviso Field Generator: A light-bending and sensor-absorbing field that renders the Defender effectively invisible to all known 20th and 21st-century detection methods.
Isomorphic Projection System: Emergency holographic projectors capable of generating hard-light, semi-sentient constructs for repair, maintenance, or operational support in the field.
Cargo Bay: 150 m³ of configurable space equipped with stasis-field projectors for safe transport of sensitive artifacts.
STRUCTURE & AIRFRAME
Materials: Ceramic-Composite Matrix with a woven Carbon-Nanotube subframe. Provides exceptional thermal and structural integrity.
Thermal Protection: Ablative ceramic tiles on the ventral and leading-edge surfaces for atmospheric re-entry. The rest of the airframe is designed to withstand the extreme temperatures of fusion exhaust.
Configuration: Lifting-body design based on the 20th-century Space Shuttle orbiter, optimized for atmospheric glide and hypersonic flight.
CREW & SUPPORT
Standard Crew: 1 (Chrononaut Pilot)
Support Capacity: 2 (for short-duration missions)
Life Support: Closed-loop system capable of sustaining a full crew for 30 days without resupply.
TIME Suit (Temporal Incursion Masked Entry Suit): The standard-issue flight suit for all Chrononauts, providing radiation shielding, life support, and interface with the ship's systems.
MISSION HISTORY
03.30.2084: Maiden voyage. Public exhibition launch from Kennedy Space Center, FL.
03.30.2084: Successful temporal crossover to 03.30.1984.
04.03.2084: Mission completion. Successful return to 2084 with full cargo and apprehended fugitive Chim-Sum Dippe. All mission objectives met.
//END OF FILE//
Launch Profile:
"The Screamer"
This is the operational timeline for a runway launch of the ship, from brake release to the moment it hits 880 mph on the way back down.
Phase 1: The Ascent (0 to 58 seconds)
T-0 to T-5 seconds: Full throttle is applied. The three TRS 25 engines, generating a combined 414,000 lbs of thrust, slam the 331,000-pound vehicle down the runway. The 1.25 thrust-to-weight ratio ensures it's airborne in seconds.
T-5 seconds: The ship pitches up violently, transitioning from horizontal flight to a vertical climb.
T-5 to T-58 seconds: The engines continue at full power, burning the high-energy propellant at a rate of 535.5 kg/s. The ship's acceleration increases as its mass plummets, rocketing it through the atmosphere.
T = 58 seconds: The engines shut down. The ship has just reached its 100 km apogee. It hangs momentarily in the blackness of space, weightless and silent.
Phase 2: The Dive (58 to 79 seconds)
T = 58 seconds: The pilot orients the craft for a nose-down vertical dive and re-ignites the engines.
T = 58 to T = 79.2 seconds:The ship accelerates downward under the combined force of gravity and its engines, reaching a net acceleration of approximately 2 Gs.
T = 79.2 seconds: The ship's velocity hits 880 mph (Mach 1.3). This is the moment the pilot must act.
Phase 3: The Window (79 to 84 seconds)
T = 79.2 to T = 81.2 seconds:For exactly three seconds, the ship maintains its 880 mph speed while the pilot manually activates the next system.
T = 81.2 seconds: The pilot's action is complete.
T = 81.2 to T = 83.2 seconds:A built-in two-second system lag passes as the next sequence initializes.
T = 83.2 seconds: The "next event" begins.
Total Mission Time
Time to Apogee: 58 seconds
Time to 880 mph: 21.2 seconds (from apogee)
Total Time from Launch to "Next Event": 83.2 seconds
This ship gets where it needs to go in one minute and is screaming back down, ready for the next maneuver, in another minute and a half.
It is an absolute beast of performance engineering.
CLASSIFIED INTERNAL ADDENDUM: DEFENDER SSTO CAPABILITY ANALYSIS
//FOR INTERNAL EYES ONLY//
SUBJECT: Verification of Multi-Launch SSTO Mission Profile
1. Propellant Mass Analysis:
Baseline Chemical Requirement: 31,081 kg (per single SSTO ascent).
Fusion Drive Efficiency Factor: 100x (conservative estimate).
Propellant per Full Flight Cycle: 311 kg.
Standard Onboard Load:4,000 kg (provides for ~12 full flight cycles with safety margin).
2. Launch Mass Calculation:
Dry Mass: 69,000 kg
Standard Propellant Load:4,000 kg
Maximum Mission Payload:6,500 kg
Total Launch Mass: 79,500 kg (175,000 lbs)
3. Engine Performance (TRS-25 Fusion):
Required Thrust (T/W Ratio 1.25): ~973,875 N
Total Engine Output: 219,000 lbs
Per-Engine Thrust (x3):~73,000 lbs
4. "Phoenix" Mission Profile (Multi-Launch Capability):
Capability: The Defender can perform a minimum of 12 full launch and landing cycles from a standard propellant load.
Propellant Consumption:~311 kg per cycle.
Post-Mission State: After 12 cycles, approximately 268 kg of propellant reserve remains for on-orbit maneuvering and contingency.
Phoenix & Vanguard System Overview & Launch
Cavalry Time Shuttles, designation TTS-02 "Phoenix", and TTS-03 "Vanguard" represent the groundbreaking innovation of temporal transportation technology applied to special operations.
Combining advanced Tachyon-8 particle manipulation with state-of-the-art navigation systems and a specialized defense payload with modular cargo bay configurable for each mission. Currently fitted for personnel rescue on Planet X.
Current Launch System:"The Screamer" (See Mission Overview)
Flight & Temporal Operations
Descent & Time Barrier Penetration: At apogee, the TRS-25 engines ignite to achieve hypersonic velocity. When terminal velocity is reached (approximately 765 knots), the Tachyon drive is activated and propels the vehicle across the time barrier. These Time Shuttles use oscillation phasing to maneuver in the static continuum using conventional propulsion. They can remain in the temporal medium for the duration that Tachyon-8 particles remain, and they land conventionally in both normal space and the temporal medium.
Return Journey: The Time Shuttles use remaining liquid fuel to launch from ground level, achieve transonic speed on a cross-gravitational shear vector, and at 765 knots (880 MPH), the pilot engages the Tachyon drive to time-warp.
Temporal Navigation Rate: The Prototype Time Shuttles can achieve navigation through the continuum laterally, without being subject to the passage of time.
Physical Specifications & Cargo
Total Weight: Approximately 90 metric tons
Cargo Bay Dimensions: 20 meters long, ~5 meters diameter
Standard Cargo Capacity: Approx. 6.8 metric tons
Maximum Payload: 50 metric tons
Weight and other specifics on equipment and fuel for the Tachyon drive are classified, but are thought to require the additional cargo capacity.
Core Systems
Temporal Core: Mallet Compensation Waveform Generator
Power Source: Tachyon-8 Particle Chamber
Navigation: Graviton-Aligned Temporal GPS
Life Support: Advanced Environmental Control System
Hull: Temporal Displacement Resistant Alloy
Safety Systems
Temporal Shielding: Prevents paradox exposure
Emergency Return Protocol: Automatic return to origin point
Quantum Stabilizers: Maintains temporal coherence
Paradox Detection Array: Early warning system
Mission Parameters
Primary Mission: Tactical Response, SAR, Recovery, Extraction, Evacuation.
Secondary Objectives: Timeline observation and paradox prevention.
Maximum Temporal Displacement: -0 years (Lateral time travel only).
Crew Capacity: 1 pilot, 70 passengers.
U.S. TEMPORAL AGENCY // TECHNICAL BRIEFING
TIME CAVALRY PROTOTYPES: PHOENIX (TTS-02) & VANGUARD (TTS-03)
//CLASSIFICATION: LEVEL 3 CHRONO-SECRET//EYES ONLY// //DOCUMENT ID: USTA-TS-CAVALRY-2084-SPEC-V1.0// //LAST REVISED: 02.15.2084//
OVERVIEW: In response to the emerging need for a rapid-response temporal defense capability, the U.S. Temporal Agency has authorized the development of two prototype vehicles based on the Defender spaceframe. The Time Cavalry prototypes, Phoenix (TTS-02) and Vanguard (TTS-03), are specialized craft designed for lateral temporal jumps and tactical deployment, rather than long-duration historical preservation missions.
DESIGN PHILOSOPHY: Where the Defender is an archivist's scalpel, the Phoenix and Vanguard are a surgeon's emergency kit. Their design prioritizes speed, maneuverability, and combat readiness over cargo capacity and long-term life support. They are built to get a team of specialists into a temporal crisis zone fast, execute their mission, and get out.
PROPULSION SYSTEM: MODIFIED TRS-25F
The prototypes are equipped with a variant of the TRS-25 fusion drive, designated TRS-25F (F for "Fast").
Key Modification: The T8 injection matrix has been retuned for rapid energy cycling, enabling near-instantaneous temporal crossover initiation.
Trade-off: This modification increases T8 particle consumption by 40% and significantly reduces engine lifespan, making it unsuitable for long-duration missions but ideal for short, sharp jumps.
Thrust Output: Remains comparable to the base TRS-25 model.
PERFORMANCE METRICS
Launch Configuration Mass:118,000 kg (260,145 lbs)
Dry Mass (Structure & Systems): 68,000 kg
Onboard Propellant (Standard Load): 2,000 kg
Maximum Mission Payload: 8,000 kg (Crew, gear, and light support equipment)
Temporal Crossover:Optimized for lateral (sideways) time jumps. Standard operational range is a 5-year temporal variance with a maximum single-jump limit of 10 years. The system requires a 15-minute cooldown and recalibration between jumps.
Atmospheric Flight:Increased atmospheric performance with a maximum velocity of Mach 4+. Enhanced maneuvering thrusters provide superior agility in atmospheric and low-orbit environments.
MISSION SYSTEMS
Offensive Systems: Equipped with a forward-mounted kinetic energy pulser and a modular hardpoint system for mission-specific weapon packages (e.g., non-lethal sonic emitters, EMP generators).
Defensive Systems: Features an upgraded Inviso Field Generator with a "flicker" capability for rapid tactical repositioning. Ablative armor plating has been added to key sections of the hull for increased resilience.
Crew & Support:
Standard Crew: 2 (Pilot & Systems Officer)
Support Capacity: 4 (Time Cavalry Specialists)
Life Support: 7-day closed-loop system, designed for short-duration missions.
Cargo Bay: 30 m³, primarily configured for weapons deployment, tactical gear, and a limited medical bay.
PROTOTYPE-SPECIFIC DIFFERENCES
TTS-02 PHOENIX (Lead Ship)
Role: Pilot Training & Pathfinding. The Phoenix is the lead test vehicle, equipped with enhanced sensors and data-recording equipment to map and validate new temporal jump vectors.
Configuration: Features a slightly larger cockpit to accommodate a flight instructor for training missions.
TTS-03 VANGUARD (Wingman)
Role: Tactical Assault & Electronic Warfare. The Vanguard is the combat-ready prototype, carrying a heavier weapons and electronic countermeasures loadout.
Configuration: Features a dedicated co-pilot/Systems Officer station with advanced controls for managing the ship's expanded combat and defense suites.
DEVELOPMENTAL STATUS: Both the Phoenix and Vanguard have completed ground testing and low-orbit flight trials. They are scheduled for full operational readiness drills in preparation for their first official deployment.
//END OF FILE//
The Final Mass Budget Breakdown
Here is the complete accounting for the ship's mass at liftoff, incorporating the first mission's specific cargo:
Ship's Dry Mass (The "Bus"):69,000 kg
This is the base weight of the orbiter itself: structure, skin, landing gear, avionics, life support, and the three TRS 25 engines.
Propellant (The "Go-Fast Juice"): 31,081 kg
This is the super-efficient 2083 propellant needed for the ascent and dive. It is stored in the ship's internal tanks, which are part of the dry mass.
Specialized Equipment: 1,000 kg (1 metric ton)
This is part of your cargo payload. It could be anything from scientific gear to the power supply and control units for the arcade games.
The Corvette: ~1,500 kg
A base model C4 Corvette has a curb weight of approximately 1,450 kg. We'll use a round 1,500 kg.
Fifty 80s Arcade Games:~4,000 kg
A classic arcade cabinet is heavy. They easily weigh around 80 kg (175 lbs) each.
50 games × 80 kg/game = 4,000 kg.
The Final Tally
For the exhibition mission, how much of the 50,000 kg cargo capacity is used:
Cargo Used:
Specialized Equipment: 1,000 kg
Corvette: 1,500 kg
Arcade Games: 4,000 kg
Total Cargo Mass = 6,500 kg (or 6.5 metric tons)
Remaining Cargo Capacity:
50,000 kg (Max Capacity) - 6,500 kg (Cargo Used) = 43,500 kg
2084 WILL CONTINUE
in THE HANGAR
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80's Main Street was just the beginning.
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