Editing The Chimera Directive

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To provide for these objectives, the Designers recommended that the Rosenanté class starship meets or exceeds the design goals in the following specification Categories;
To provide for these objectives, the Designers recommended that the Rosenanté class starship meets or exceeds the design goals in the following specification Categories;


<font color=goldenrod>'''Propulsion'''</font>
'''Propulsion'''
* Sustainable cruise Velocity of Warp Factor 9.4. Ability to maintain speeds of up to Warp Factor 9.7 for periods of up to 12 Hours.
* Sustainable cruise Velocity of Warp Factor 9.4. Ability to maintain speeds of up to Warp Factor 9.7 for periods of up to 12 Hours.
* Sixth-phase dilithium controlled matter/antimatter reactor for primary power. Sustainable field output to exceed 1, 650 cochranes, peak transitional surge reserve to exceed 4,225% of nominal output. (170ns phase)
* Sixth-phase dilithium controlled matter/antimatter reactor for primary power. Sustainable field output to exceed 1, 650 cochranes, peak transitional surge reserve to exceed 4,225% of nominal output. (170ns phase)
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* Secondary (impulse) propulsion systems to provide sub-light velocities up to and including .92 light speed (c). Engine systems of choice to include but not limited to at least two YPS 8063 fusion drive motors. All units to be equipped with subspace drive accelerators, field output not less than 180 millicochranes at 1.02 X l0³K. Reactor Modules to be field replaceable.
* Secondary (impulse) propulsion systems to provide sub-light velocities up to and including .92 light speed (c). Engine systems of choice to include but not limited to at least two YPS 8063 fusion drive motors. All units to be equipped with subspace drive accelerators, field output not less than 180 millicochranes at 1.02 X l0³K. Reactor Modules to be field replaceable.


<font color=goldenrod>'''Mission'''</font>
'''Mission'''
* Ability to operate independent of Starbase refurbishment for moderate periods of time. Independent operation mode capability of 1 Standard years at nominal Warp 6. Ability to execute deep-space exploration missions including charting and mapping, hostile contact scenarios, intelligence gathering and infiltration missions, full technical, biological and ecological studies.
* Ability to operate independent of Starbase refurbishment for moderate periods of time. Independent operation mode capability of 1 Standard years at nominal Warp 6. Ability to execute deep-space exploration missions including charting and mapping, hostile contact scenarios, intelligence gathering and infiltration missions, full technical, biological and ecological studies.
* Ability to support a wide range of mission-related ongoing research and other projects without impact on primary mission operations.
* Ability to support a wide range of mission-related ongoing research and other projects without impact on primary mission operations.
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* Support facilities for auxiliary spacecraft and instrumented probes for short-range operations to include at least 1 independent launch, resupply, and repair bays.
* Support facilities for auxiliary spacecraft and instrumented probes for short-range operations to include at least 1 independent launch, resupply, and repair bays.


<font color=goldenrod>'''Environment/Crew'''</font>
'''Environment/Crew'''
* Environmental systems to conform to Starfleet Regulatory Agency (SFRA)- standard 102.9 for Class M compatible oxygen breathing personnel. All life-critical systems to be triply redundant. Life support modules to be replaceable at major Starbase layover to permit vehicle-wide adaptation to Class H, K or L environmental conditions.
* Environmental systems to conform to Starfleet Regulatory Agency (SFRA)- standard 102.9 for Class M compatible oxygen breathing personnel. All life-critical systems to be triply redundant. Life support modules to be replaceable at major Starbase layover to permit vehicle-wide adaptation to Class H, K or L environmental conditions.
* Ability to support up to 200 non-crew personnel for mission related operations.
* Ability to support up to 200 non-crew personnel for mission related operations.
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* All habitable volumes to be protected to SFRA-standard 347.3(a) levels for EM and radiation. Subspace flux differential to be maintained within 0.02 millicochranes.
* All habitable volumes to be protected to SFRA-standard 347.3(a) levels for EM and radiation. Subspace flux differential to be maintained within 0.02 millicochranes.


<font color=goldenrod>'''Tactical'''</font>
'''Tactical'''
* Defensive Shielding to exceed 9.85 X 103 kW primary energy dissipation rate. All tactical Shielding to have full redundancy, with auxiliary system able to provide 75% of primary rating.
* Defensive Shielding to exceed 9.85 X 103 kW primary energy dissipation rate. All tactical Shielding to have full redundancy, with auxiliary system able to provide 75% of primary rating.
* Tactical systems to include full array of Type XII phaser bank elements on hull capable of 6.1MW maximum single emitter output. 6 Photon Torpedo launchers required for ship defensive capabilities.
* Tactical systems to include full array of Type XII phaser bank elements on hull capable of 6.1MW maximum single emitter output. 6 Photon Torpedo launchers required for ship defensive capabilities.
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* Tactical systems to include variable EM field dampening systems to reduce or eliminate vessel EM fields and signatures.
* Tactical systems to include variable EM field dampening systems to reduce or eliminate vessel EM fields and signatures.


<font color=goldenrod>'''Design Life'''</font>
'''Design Life'''
* Space frame design life of approximately 100 years, assuming approximately 5 major ship- wide system swap outs and upgrades at average intervals of 20 years. Such upgrades help ensure the continuing usefulness of the ship even though significant advances in technology are anticipated during that time. Minor refurbishment and upgrade to occur at approximately one- to five year intervals, depending on specific mission requirements and hardware availability.
* Space frame design life of approximately 100 years, assuming approximately 5 major ship- wide system swap outs and upgrades at average intervals of 20 years. Such upgrades help ensure the continuing usefulness of the ship even though significant advances in technology are anticipated during that time. Minor refurbishment and upgrade to occur at approximately one- to five year intervals, depending on specific mission requirements and hardware availability.


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