ArmorandClaude Opus 4.7
3cfbf8433d
- Replace RS-25E with RS-25EX throughout (2.88 t, 26 MPa, 2812 kN, 454 s vac / 2353.7 kN, 380 s SL) - Dry mass 111.6 t → 110.5 t; burn time 10m16s → 8m30s normal / 12m extended - Rewrite abort section: 6 modes (add Hard Abort), detailed main engine engine-out scenario (100 t to 650×650 km, 28° from Wenchang) - Add booster engine-out section (TH-12 tolerance, downrange/recovery abort, T+60s worst case → RTLS / Hard Abort) - Fix ST-02 reference: 万星源NEXT号 → 克丽斯腾号 Co-Authored-By: Claude Opus 4.7 <noreply@anthropic.com>
387 lines
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387 lines
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<article class="mw-parser-output wiki-article">
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<h1 id="vulture-shuttle">Vulture Shuttle</h1>
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<table class="infobox">
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<caption>Vulture Shuttle<span>秃鹫航天飞机</span></caption>
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<tbody>
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<tr><td><a class="media-link" href="#vulture-img-stack"><img src="/vulture/vulture_shuttle_full_stack_original.png" alt="Vulture Shuttle full launch stack" data-wiki-asset="/vulture/vulture_shuttle_full_stack_original.png"></a><div class="thumbcaption">The Vulture Shuttle stack consists of the MK4 orbiter, an external tank, and two reusable liquid boosters.</div></td></tr>
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<tr><td><b>Type</b>: Partially reusable heavy shuttle system</td></tr>
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<tr><td><b>Lineage</b>: STS Shuttle - CERV Shuttle - Vulture Shuttle</td></tr>
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<tr><td><b>Predecessor</b>: CERV Shuttle</td></tr>
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<tr><td><b>Development start</b>: 2030</td></tr>
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<tr><td><b>First flight</b>: March 2037 (VLT-01, uncrewed orbital test, VS-01 <i>Endurance</i>)</td></tr>
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<tr><td><b>Entered service</b>: 2039</td></tr>
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<tr><td><b>Main launch site</b>: Wenchang</td></tr>
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<tr><td><b>Typical target orbit</b>: 1000 km x 1000 km, 45 degrees</td></tr>
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<tr><td><b>Block 1 payload</b>: 100 t to the typical target orbit</td></tr>
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<tr><td><b>Zero-payload liftoff mass</b>: 4065.9 t</td></tr>
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<tr><td><b>Liftoff thrust</b>: 61,949 kN</td></tr>
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<tr><td><b>Maximum crew</b>: 19</td></tr>
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<tr><td><b>Status</b>: In service</td></tr>
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<tr><td><b>Total flights</b>: 2,266 (through March 2060)</td></tr>
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</tbody></table>
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<p>The <b>Vulture Shuttle</b> is the third major vehicle in the STS Shuttle - CERV Shuttle - Vulture Shuttle lineage in this alternate spaceflight timeline. It keeps the classic orbiter, external tank, and side-booster arrangement, but replaces solid boosters with reusable liquid boosters and scales the orbiter into the large MK4 class.</p>
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<p>Vulture development began in 2030 as a heavy successor to CERV. The first uncrewed orbital test flight, VLT-01, launched in March 2037 aboard VS-01 <i>Endurance</i>. The system entered operational service in 2039 and became the primary shuttle-line heavy transport after CERV retirement in 2040. By March 2060 the fleet had accumulated 2,266 flights across ten orbiters in three blocks.</p>
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<nav class="toc" aria-label="Contents">
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<div class="toc-title">Contents</div>
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<ol>
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<li><a href="#development">Development</a></li>
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<li><a href="#system-components">System components</a></li>
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<li><a href="#mission-profile">Mission profile</a></li>
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<li><a href="#fleet">Fleet</a></li>
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<li><a href="#operational-history">Operational history</a></li>
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<li><a href="#block-15">Block 1.5</a></li>
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<li><a href="#block-2">Block 2</a></li>
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<li><a href="#safety-and-incidents">Safety and incidents</a></li>
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<li><a href="#launch-history">Launch history</a></li>
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<li><a href="#specifications">Specifications</a></li>
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<li><a href="#images">Images</a></li>
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<li><a href="#see-also">See also</a></li>
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</ol>
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</nav>
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<h2 id="development">Development</h2>
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<p>The alternate timeline diverges from real-world shuttle history after the Columbia accident, which still occurs in 2003 and becomes the central safety lesson for later shuttle development. The CERV Shuttle, developed from 2005 and first flown in 2015, extends the shuttle lineage with an integrated crew-cabin escape system, modern avionics, and improved maintainability. CERV operated from 2017 to 2040, accumulating 666 flights.</p>
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<p>Vulture development begins in 2030 as a heavier successor to CERV. Instead of being a modest safety upgrade, it is designed for heavy high-orbit logistics, large station modules, and the assembly of interplanetary exploration motherships. Key choices include an enlarged MK4 orbiter, a 10 m external tank, reusable 5 m liquid boosters, and an expanded crew escape concept inherited from CERV. The first Block 1 orbiter, VS-01 <i>Endurance</i>, conducted its maiden uncrewed orbital flight in March 2037. After a two-year test and certification campaign, Vulture entered operational service in 2039. CERV was fully retired in 2040, completing the handover to the third-generation shuttle.</p>
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<h2 id="system-components">System components</h2>
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<h3 id="orbiter">Orbiter</h3>
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<figure class="thumb tright"><a class="media-link" href="#vulture-img-ascent"><img src="/vulture/vulture_ascent_original.png" alt="Vulture Shuttle during ascent" data-wiki-asset="/vulture/vulture_ascent_original.png"></a><figcaption class="thumbcaption">The MK4 orbiter uses a large delta wing, wingtip vertical tails, canards, and a retractable nose docking port.</figcaption></figure>
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<p>The MK4 orbiter is the crew, payload, and on-orbit operations core of the system. It has a large delta wing, wingtip vertical tails, forward canards, a pressurized crew cabin, a large cargo bay, OMS/RCS propulsion, two atmospheric jet engines, and five RS-25EX main engines fed by the external tank during ascent.</p>
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<p>The <b>RS-25EX</b> is an evolution of the RS-25DX, with development beginning in 2020. Key improvements over the RS-25DX include extensive use of 3D printing, which reduced the parts count by approximately 40%, and the replacement of selected Inconel components with ceramic-matrix composites (CMC) for weight reduction. Each RS-25EX has a dry mass of 2.88 t and a chamber pressure of 26 MPa. It produces 2,812 kN of thrust at a vacuum specific impulse of 454 s. Sea-level performance is substantially improved over earlier RS-25 variants, delivering 2,353.7 kN at 380 s specific impulse. The nominal maximum continuous burn time is 8 minutes 30 seconds, extendable to 12 minutes when multiple engine-out conditions require extended burning on the remaining engines.</p>
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<p>The payload bay can accommodate cargo about 5.4 m long, 7.75 m wide, and 29.5 m high. This makes Vulture especially useful for wide station modules, large radiators, truss sections, and mothership components that are difficult to package inside cylindrical expendable fairings.</p>
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<h3 id="external-tank">External tank</h3>
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<p>The external tank stores liquid oxygen and liquid hydrogen for the orbiter's main engines. It is 10 m in diameter, carries 1612.2 t of propellant, and has a dry mass of 31.5 t. Unlike the STS external tank, it uses a lower-shedding insulation coating rather than traditional foam in order to reduce debris risk to the orbiter thermal protection system.</p>
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<h3 id="liquid-boosters">Liquid boosters</h3>
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<figure class="thumb tleft"><a class="media-link" href="#vulture-img-recovery"><img src="/vulture/vulture_booster_recovery_original.png" alt="Vulture liquid booster recovery" data-wiki-asset="/vulture/vulture_booster_recovery_original.png"></a><figcaption class="thumbcaption">The liquid boosters return to the launch site after separation and land propulsively.</figcaption></figure>
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<p>Two 5 m liquid boosters provide most liftoff thrust. Each booster carries 19 Tianhuo-12 LOX/kerosene engines, burns for about 135 seconds, then separates and performs RTLS recovery using grid fins, hot-gas RCS, landing legs, and propulsive landing.</p>
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<h2 id="mission-profile">Mission profile</h2>
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<figure class="thumb tright"><a class="media-link" href="#vulture-img-separation"><img src="/vulture/vulture_booster_separation_original.png" alt="Vulture liquid booster separation" data-wiki-asset="/vulture/vulture_booster_separation_original.png"></a><figcaption class="thumbcaption">After booster cutoff, the reusable liquid boosters separate and return to the launch site while the orbiter and external tank continue upward.</figcaption></figure>
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<p>During ascent, the liquid boosters and five RS-25EX main engines operate together. After booster cutoff and separation, the boosters return to the launch site while the orbiter and external tank continue to a high suborbital insertion. After main engine cutoff, the orbiter separates from the external tank and uses OMS burns to enter and raise its orbit.</p>
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<h3 id="abort-modes">Abort Modes</h3>
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<p>The Vulture Shuttle relies on its five RS-25EX engines and generous OMS margins to provide a graduated abort hierarchy that escalates with the severity of the failure. The actual mode triggered depends on how many engines have been lost, when in ascent the failures occur, and the vehicle's instantaneous thrust-to-weight ratio. Six abort modes are defined, ordered from least to most severe:</p>
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<ul>
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<li><b>Abort to Orbit</b> — The remaining main engines push the orbiter into a near-nominal orbit; the OMS takes over from there to complete or adjust the mission.</li>
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<li><b>On Orbit Abort</b> — The main engines can no longer deliver the mission, but the OMS alone can reach orbit. The payload is placed into a 400 km × 400 km parking orbit when conditions permit, and the vehicle returns at the earliest opportunity.</li>
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<li><b>Abort Once Around</b> — The orbiter completes one full revolution and returns, jettisoning the payload in orbit to reduce landing weight.</li>
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<li><b>Trans-Ocean Abort</b> — Orbital insertion is out of reach. The vehicle uses its remaining energy to attempt a landing at a civilian airfield across the ocean.</li>
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<li><b>RTLS Abort</b> — The vehicle reverses course immediately and returns to the launch site.</li>
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<li><b>Hard Abort</b> — Controlled flight is no longer possible (Loss of Vehicle). The crew cabin separates from the orbiter, stabilizes, and descends under drogue and main parachutes. This is the last-resort layer, triggered only when every other abort mode is unavailable.</li>
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</ul>
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<h3 id="main-engine-engine-out">Main Engine Engine-Out</h3>
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<p>The following analysis uses a representative Block 1 mission: 100 t payload launched from Wenchang, targeting a 650 km × 650 km circular orbit at 28° inclination. All TWR values refer to the vehicle's instantaneous thrust-to-weight ratio at the moment of failure.</p>
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<h4>One RS-25EX shutdown immediately after liftoff</h4>
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<p>With no further RS-25EX failures, the remaining four engines deliver the stack into a 30 km × 650 km transfer orbit. The mission continues without deviation.</p>
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<ul>
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<li>Before TWR reaches 1: loss of any additional engine → <b>RTLS Abort</b>.</li>
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<li>Before TWR reaches 1.15: loss of an additional engine → <b>On Orbit Abort</b>. The OMS can complete insertion, but the vehicle should return promptly; the payload is typically placed into a 350 km × 650 km orbit beforehand.</li>
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<li>After TWR reaches 1.15: loss of an additional engine → <b>Abort to Orbit</b>.</li>
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<li>After TWR reaches 1.8: the vehicle can absorb two consecutive additional shutdowns (three total failures) with the mission continuing nominally.</li>
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<li>After TWR reaches 1.8: loss of three additional engines (four total failures) → <b>Trans-Ocean Abort</b> or <b>Abort Once Around</b>, based on remaining energy and ground-track geometry.</li>
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</ul>
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<h4>Normal ascent timeline</h4>
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<ul>
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<li><b>T+3 min 45 s</b> (or TWR ≥ 1.15): can sustain two consecutive shutdowns → <b>Abort to Orbit</b>.</li>
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<li><b>T+4 min</b> (or TWR ≥ 1.2): can sustain two shutdowns and still reach a nominal orbit.</li>
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<li><b>T+5 min 45 s</b> (or TWR ≥ 1.75): can sustain three consecutive shutdowns and still reach a nominal orbit. One further shutdown → <b>Trans-Ocean Abort</b> or <b>Abort Once Around</b>.</li>
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</ul>
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<h3 id="booster-engine-out">Booster Engine-Out</h3>
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<p>Each liquid booster carries 19 Tianhuo-12 (TH-12) LOX/kerosene engines and has its own engine-out tolerance: a single booster can absorb up to two TH-12 shutdowns with no effect on the mission.</p>
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<p>When a single booster loses 2 to 6 TH-12 engines, the affected side forgoes its recovery attempt. The opposite booster matches the shutdown count to preserve thrust symmetry, and both boosters extend their burn to compensate for the lost impulse. The mission proceeds normally; only the booster recovery is scrubbed.</p>
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<p>Beyond 6 TH-12 shutdowns, the flight computer evaluates the vehicle's remaining energy and trajectory to select the appropriate abort mode from the hierarchy above.</p>
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<p>The most severe booster case occurs <b>before T+60 seconds</b>, when one booster loses thrust entirely. If all five RS-25EX engines are healthy, the boosters are commanded to shut down, the vehicle coasts through max-Q, the boosters are jettisoned, and the orbiter flies an <b>RTLS maneuver</b> back to the launch site. If any single RS-25EX has also failed at this point, the vehicle is declared unrecoverable (Loss of Vehicle) and <b>Hard Abort</b> is triggered immediately — the crew cabin separates and descends under parachutes.</p>
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<h2 id="fleet">Fleet</h2>
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<p>Ten Vulture orbiters have been built across three blocks. Five Block 1 orbiters have been retired, two Block 1.5 orbiters are currently active, and three Block 2 orbiters are currently active. Flight rates are approximately 12 flights per year per Block 1 orbiter, 24 per year per Block 1.5 orbiter, and 48 per year per Block 2 orbiter.</p>
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<h3 id="fleet-block1">Block 1 (Retired)</h3>
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<table>
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<thead><tr><th>Vehicle</th><th>Name</th><th>Service Period</th><th>Total Flights</th><th>Status</th></tr></thead>
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<tbody>
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<tr><td>VS-01</td><td><i>Endurance</i></td><td>2037-03 to 2057-06</td><td>240</td><td>Retired</td></tr>
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<tr><td>VS-02</td><td><i>Perseverance</i></td><td>2038-01 to 2057-11</td><td>235</td><td>Retired</td></tr>
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<tr><td>VS-03</td><td><i>Courage</i></td><td>2039-05 to 2058-03</td><td>240</td><td>Retired</td></tr>
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<tr><td>VS-04</td><td><i>Determination</i></td><td>2040-02 to 2058-08</td><td>228</td><td>Retired</td></tr>
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<tr><td>VS-05</td><td><i>Patience</i></td><td>2041-07 to 2056-12</td><td>132</td><td>Retired</td></tr>
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</tbody></table>
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<p>VS-05 <i>Patience</i> underwent a nuclear thermal OMS conversion in 2048, which reduced its flight rate compared to other Block 1 vehicles. All five Block 1 orbiters operated at a nominal rate of 12 flights per year. The Block 1 fleet accumulated 1,075 flights before the last vehicle retired in August 2058.</p>
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<h3 id="fleet-block15">Block 1.5 (Active as of March 2060)</h3>
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<table>
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<thead><tr><th>Vehicle</th><th>Name</th><th>Block 1 Period</th><th>Conversion</th><th>Block 1.5 Period</th><th>Flights (B1/B1.5)</th><th>Status</th></tr></thead>
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<tbody>
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<tr><td>VS-06</td><td><i>Fortitude</i></td><td>2042 to 2051</td><td>2051-2052</td><td>2052 to present</td><td>305 (108 / 197)</td><td>Active</td></tr>
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<tr><td>VS-07</td><td><i>Loyalty</i></td><td>2043 to 2052</td><td>2052-2053</td><td>2053 to present</td><td>280 (108 / 172)</td><td>Active</td></tr>
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</tbody></table>
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<p>VS-06 <i>Fortitude</i> and VS-07 <i>Loyalty</i> were originally built as Block 1 vehicles and served in that configuration for approximately nine years each. Both were converted to Block 1.5 standard with nuclear aerospike propulsion and continue to operate at approximately 24 flights per year each.</p>
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<h3 id="fleet-block2">Block 2 (Active as of March 2060)</h3>
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<table>
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<thead><tr><th>Vehicle</th><th>Name</th><th>Service Period</th><th>Total Flights</th><th>Status</th></tr></thead>
|
|
<tbody>
|
|
<tr><td>VS-08</td><td><i>Honor</i></td><td>2055-03 to present</td><td>250</td><td>Active</td></tr>
|
|
<tr><td>VS-09</td><td><i>Conviction</i></td><td>2056-06 to present</td><td>202</td><td>Active</td></tr>
|
|
<tr><td>VS-10</td><td><i>Hope</i></td><td>2057-08 to present</td><td>154</td><td>Active</td></tr>
|
|
</tbody></table>
|
|
<p>All three Block 2 vehicles operate at approximately 48 flights per year each. Built with nuclear aerospike propulsion from the start, they carry about 120 t to low lunar orbit and are the primary heavy-lift vehicles for the current fleet.</p>
|
|
<h2 id="operational-history">Operational history</h2>
|
|
<p>Vulture's first flight, VLT-01, launched in March 2037 with VS-01 <i>Endurance</i> on an uncrewed orbital test mission. VS-02 <i>Perseverance</i> joined the fleet in January 2038. After a two-year test and certification campaign, Vulture entered operational service in 2039, with VS-03 <i>Courage</i> joining that May. VS-04 <i>Determination</i> followed in February 2040, and CERV completed its handover with retirement the same year.</p>
|
|
<p>Through the 2040s, the Block 1 fleet expanded to seven vehicles with the addition of VS-05 <i>Patience</i> (July 2041), VS-06 <i>Fortitude</i> (2042), and VS-07 <i>Loyalty</i> (2043). With seven Block 1 orbiters each flying approximately 12 times per year, the fleet achieved an annual rate of about 84 flights. VS-05 underwent a nuclear thermal OMS conversion in 2048, pioneering high-energy propulsion integration on the MK4 airframe, though this reduced its flight rate for the remainder of its career.</p>
|
|
<p>During the 2040s and early 2050s, Vulture supported large orbital facilities and the construction of exploration motherships, including Xihe (XH-01), Stellaria (ST-01), and the second early ST-series Stellaria-class ship (ST-02). The fleet reached its peak Block 1 tempo in the late 2040s.</p>
|
|
<p>In 2051, VS-06 <i>Fortitude</i> was withdrawn from Block 1 service for conversion to Block 1.5 standard, completing the process in 2052. VS-07 <i>Loyalty</i> followed, converting between 2052 and 2053. The Block 1.5 vehicles operate at approximately 24 flights per year each, roughly double the Block 1 rate.</p>
|
|
<p>The Block 2 era began in March 2055 with the first flight of VS-08 <i>Honor</i>, followed by VS-09 <i>Conviction</i> in June 2056 and VS-10 <i>Hope</i> in August 2057. Block 2 vehicles operate at approximately 48 flights per year each. The Block 1 fleet phased out during 2056-2058, with VS-05 retiring in December 2056, VS-01 in June 2057, VS-02 in November 2057, VS-03 in March 2058, and VS-04 in August 2058.</p>
|
|
<p>As of March 2060, the active fleet consists of five vehicles: two Block 1.5 (VS-06, VS-07) and three Block 2 (VS-08, VS-09, VS-10), with the fleet having accumulated a total of 2,266 flights.</p>
|
|
<p>The Echo Shuttle (first flight 2056, operational 2057) and Enterprise Shuttle (first flight 2057, operational 2058) have since joined the shuttle lineage as fourth-generation SSTO-capable vehicles, complementing the Vulture fleet in the late 2050s.</p>
|
|
<h2 id="block-15">Block 1.5</h2>
|
|
<p>Block 1.5 is a high-energy propulsion conversion of the VS-06 and VS-07 Block 1 orbiters. It installs nuclear aerospike engines and modifies propellant management, thermal isolation, aft structure, flight software, and ground safety procedures. Its core ability is SSTO operation, but payload is reduced to about 40 t. Conversion of each vehicle takes approximately one year. Flight rate increases from the Block 1 baseline of 12 to approximately 24 flights per year per orbiter.</p>
|
|
<h2 id="block-2">Block 2</h2>
|
|
<p>Block 2 is a later production standard rather than a simple conversion. VS-08, VS-09, and VS-10 are built around nuclear aerospike propulsion, deep-space communications, high-energy propellant management, and stricter re-entry limits. Block 2 can carry about 120 t directly to low lunar orbit and return, but return payload is limited to about 40 t and requires braking to low-Earth-orbit-class re-entry speed. Block 2 vehicles operate at approximately 48 flights per year each. First flight was VS-08 <i>Honor</i> in March 2055.</p>
|
|
<h2 id="safety-and-incidents">Safety and incidents</h2>
|
|
<figure class="thumb tright"><a class="media-link" href="#vulture-img-ignition"><img src="/vulture/vulture_shuttle_ignition_original.png" alt="Vulture Shuttle engine ignition" data-wiki-asset="/vulture/vulture_shuttle_ignition_original.png"></a><figcaption class="thumbcaption">Pad abort logic was a central part of the Vulture safety case, especially before booster ignition.</figcaption></figure>
|
|
<p>Vulture's safety design responds directly to STS-era risks: solid boosters are replaced by throttleable liquid boosters, external-tank insulation shedding is reduced, orbiter leading edges and belly tiles are instrumented, and the crew cabin can separate as an escape module in a wider range of emergencies.</p>
|
|
<table>
|
|
<thead><tr><th>Mission</th><th>Year</th><th>Event</th><th>Outcome</th></tr></thead>
|
|
<tbody>
|
|
<tr><td>VLT-02</td><td>2037</td><td>Pad abort after RS-25EX sensor disagreement</td><td>Main engines shut down before booster ignition</td></tr>
|
|
<tr><td>VLT-14</td><td>2038</td><td>Abort to Orbit after two early RS-25EX shutdowns</td><td>Safe parking orbit and early return</td></tr>
|
|
<tr><td>VLT-287</td><td>2045</td><td>Two RS-25EX shutdowns after T+6 minutes</td><td>Normal orbit with OMS correction</td></tr>
|
|
<tr><td>VLT-831</td><td>2053</td><td>Three RS-25EX shutdowns after T+8 minutes</td><td>Low-margin normal orbit</td></tr>
|
|
<tr><td>VLT-1135</td><td>2056</td><td>Block 2 braking anomaly before lunar-return re-entry</td><td>Return delayed and completed safely</td></tr>
|
|
</tbody></table>
|
|
<h2 id="launch-history">Launch history</h2>
|
|
<p>The Vulture fleet accumulated 2,266 flights between March 2037 and March 2060. Annual flight rate grew from 8 flights in the partial first year to a peak of 205 in 2057 as Block 2 vehicles came online. As of March 2060 the fleet is flying at an annualized rate of approximately 192 flights per year (2 Block 1.5 at 24/yr each + 3 Block 2 at 48/yr each).</p>
|
|
<div class="launch-chart" role="img" aria-label="Vulture Shuttle historical launch count chart">
|
|
<div class="launch-row launch-head"><span>Year</span><span>Flights</span><span>No.</span><span>Total</span></div>
|
|
<div class="launch-stage-label">Test and certification phase (Block 1, 1-2 orbiters)</div>
|
|
<div class="launch-row"><span>2037</span><span class="launch-track"><span class="launch-bar" style="width:4%;"></span></span><span class="launch-count">8</span><span class="launch-cumulative">8</span></div>
|
|
<div class="launch-row"><span>2038</span><span class="launch-track"><span class="launch-bar" style="width:11%;"></span></span><span class="launch-count">22</span><span class="launch-cumulative">30</span></div>
|
|
<div class="launch-row"><span>2039</span><span class="launch-track"><span class="launch-bar" style="width:16%;"></span></span><span class="launch-count">33</span><span class="launch-cumulative">63</span></div>
|
|
<div class="launch-row"><span>2040</span><span class="launch-track"><span class="launch-bar" style="width:22%;"></span></span><span class="launch-count">45</span><span class="launch-cumulative">108</span></div>
|
|
<div class="launch-stage-label">Block 1 fleet expansion (reaching 7 orbiters by 2043)</div>
|
|
<div class="launch-row"><span>2041</span><span class="launch-track"><span class="launch-bar" style="width:26%;"></span></span><span class="launch-count">54</span><span class="launch-cumulative">162</span></div>
|
|
<div class="launch-row"><span>2042</span><span class="launch-track"><span class="launch-bar" style="width:35%;"></span></span><span class="launch-count">72</span><span class="launch-cumulative">234</span></div>
|
|
<div class="launch-row"><span>2043</span><span class="launch-track"><span class="launch-bar" style="width:41%;"></span></span><span class="launch-count">84</span><span class="launch-cumulative">318</span></div>
|
|
<div class="launch-stage-label">Full Block 1 operations (7 orbiters at 12/yr each)</div>
|
|
<div class="launch-row"><span>2048</span><span class="launch-track"><span class="launch-bar" style="width:41%;"></span></span><span class="launch-count">84</span><span class="launch-cumulative">738</span></div>
|
|
<div class="launch-stage-label">Mothership construction peak / Block 1.5 conversion</div>
|
|
<div class="launch-row"><span>2052</span><span class="launch-track"><span class="launch-bar" style="width:41%;"></span></span><span class="launch-count">84</span><span class="launch-cumulative">1,068</span></div>
|
|
<div class="launch-stage-label">Block 1.5 operations begin</div>
|
|
<div class="launch-row"><span>2053</span><span class="launch-track"><span class="launch-bar" style="width:53%;"></span></span><span class="launch-count">108</span><span class="launch-cumulative">1,176</span></div>
|
|
<div class="launch-row"><span>2054</span><span class="launch-track"><span class="launch-bar" style="width:53%;"></span></span><span class="launch-count">108</span><span class="launch-cumulative">1,284</span></div>
|
|
<div class="launch-stage-label">Block 2 introduction</div>
|
|
<div class="launch-row"><span>2055</span><span class="launch-track"><span class="launch-bar" style="width:72%;"></span></span><span class="launch-count">148</span><span class="launch-cumulative">1,432</span></div>
|
|
<div class="launch-row"><span>2056</span><span class="launch-track"><span class="launch-bar" style="width:90%;"></span></span><span class="launch-count">184</span><span class="launch-cumulative">1,616</span></div>
|
|
<div class="launch-stage-label">Peak operations (Block 1 retirement, Block 2 full rate)</div>
|
|
<div class="launch-row"><span>2057</span><span class="launch-track"><span class="launch-bar" style="width:100%;"></span></span><span class="launch-count">205</span><span class="launch-cumulative">1,821</span></div>
|
|
<div class="launch-row"><span>2058</span><span class="launch-track"><span class="launch-bar" style="width:99%;"></span></span><span class="launch-count">203</span><span class="launch-cumulative">2,024</span></div>
|
|
<div class="launch-row"><span>2059</span><span class="launch-track"><span class="launch-bar" style="width:94%;"></span></span><span class="launch-count">192</span><span class="launch-cumulative">2,216</span></div>
|
|
<div class="launch-row"><span>2060</span><span class="launch-track"><span class="launch-bar" style="width:24%;"></span></span><span class="launch-count">50</span><span class="launch-cumulative"><b>2,266</b></span></div>
|
|
</div>
|
|
<p style="font-size:90%; color:#54595d;">2060 figures are through March only. Peak annual flight rate was 205 launches in 2057. The active fleet as of March 2060 consists of 2 Block 1.5 and 3 Block 2 orbiters, producing an annualized rate of approximately 192 flights.</p>
|
|
<h2 id="specifications">Specifications</h2>
|
|
<table>
|
|
<thead><tr><th>Parameter</th><th>Value</th></tr></thead>
|
|
<tbody>
|
|
<tr><td>Launch stack length</td><td>72 m</td></tr>
|
|
<tr><td>Zero-payload liftoff mass</td><td>4065.9 t</td></tr>
|
|
<tr><td>Liftoff thrust</td><td>61,949 kN</td></tr>
|
|
<tr><td>Block 1 orbiter dry mass</td><td>110.5 t</td></tr>
|
|
<tr><td>Orbiter length</td><td>61.5 m</td></tr>
|
|
<tr><td>Orbiter wingspan</td><td>43.5 m</td></tr>
|
|
<tr><td>Main engines</td><td>5 RS-25EX engines; dry mass 2.88 t each; chamber pressure 26 MPa; vacuum thrust 2,812 kN; vacuum Isp 454 s; sea-level thrust 2,353.7 kN; sea-level Isp 380 s; normal max burn 8 min 30 s, extendable to 12 min in multi-engine-out contingencies</td></tr>
|
|
<tr><td>OMS propellant</td><td>45.9 t MMH/NTO</td></tr>
|
|
<tr><td>Atmospheric jet fuel</td><td>10 t kerosene</td></tr>
|
|
<tr><td>Jet engine thrust</td><td>480 kN x 2 dry / 735.8 kN x 2 afterburning</td></tr>
|
|
<tr><td>Life support</td><td>19 people for 26 days</td></tr>
|
|
<tr><td>Cargo bay</td><td>About 5.4 m x 7.75 m x 29.5 m</td></tr>
|
|
<tr><td>External tank propellant</td><td>1612.2 t</td></tr>
|
|
<tr><td>External tank dry mass</td><td>31.5 t</td></tr>
|
|
<tr><td>Booster dry mass</td><td>46.5 t each</td></tr>
|
|
<tr><td>Booster burn time</td><td>135 s</td></tr>
|
|
</tbody></table>
|
|
<h2 id="images">Images</h2>
|
|
<table>
|
|
<thead><tr><th>Image</th><th>Content</th><th>Placement</th></tr></thead>
|
|
<tbody>
|
|
<tr><td>Full launch stack</td><td>MK4 orbiter, external tank, and two reusable liquid boosters.</td><td>Infobox</td></tr>
|
|
<tr><td>Engine ignition</td><td>Pad ignition and early abort context.</td><td>Safety</td></tr>
|
|
<tr><td>Ascent</td><td>Three-part ascent stack and MK4 wing layout.</td><td>Orbiter section</td></tr>
|
|
<tr><td>Booster recovery</td><td>RTLS recovery and propulsive landing of the liquid boosters.</td><td>Liquid boosters section</td></tr>
|
|
<tr><td>Booster separation</td><td>Booster cutoff, separation, and continuation of orbiter/external tank ascent.</td><td>Mission profile</td></tr>
|
|
</tbody></table>
|
|
<h2 id="see-also">See also</h2>
|
|
<ul>
|
|
<li>CERV Shuttle</li>
|
|
<li><a href="/home/Space_Shuttles/Vulture_Shuttle_Block_2">Vulture Shuttle Block 2</a></li>
|
|
<li><a href="/home/Space_Shuttles/Echo_Shuttle">Echo Shuttle</a></li>
|
|
<li><a href="/home/Space_Shuttles/Enterprise_Shuttle">Enterprise Shuttle</a></li>
|
|
<li><a href="/home/Exploration_Motherships/Xihe">Xihe-class interplanetary exploration mothership</a></li>
|
|
<li><a href="/home/Exploration_Motherships/Stellaria">Stellaria-class interplanetary exploration mothership</a></li>
|
|
<li>Nuclear aerospike engine</li>
|
|
</ul>
|
|
<div id="vulture-img-stack" class="wiki-modal"><div class="wiki-modal-card"><a class="modal-close" href="#">x</a><img src="/vulture/vulture_shuttle_full_stack_original.png" alt="Vulture Shuttle full launch stack" data-wiki-asset="/vulture/vulture_shuttle_full_stack_original.png"><div class="thumbcaption">Full Vulture Shuttle launch stack with the MK4 orbiter, external tank, and two liquid boosters.</div></div></div>
|
|
<div id="vulture-img-ignition" class="wiki-modal"><div class="wiki-modal-card"><a class="modal-close" href="#">x</a><img src="/vulture/vulture_shuttle_ignition_original.png" alt="Vulture Shuttle engine ignition" data-wiki-asset="/vulture/vulture_shuttle_ignition_original.png"><div class="thumbcaption">Engine ignition before launch, relevant to pad-abort procedures and early flight safety.</div></div></div>
|
|
<div id="vulture-img-ascent" class="wiki-modal"><div class="wiki-modal-card"><a class="modal-close" href="#">x</a><img src="/vulture/vulture_ascent_original.png" alt="Vulture Shuttle during ascent" data-wiki-asset="/vulture/vulture_ascent_original.png"><div class="thumbcaption">Vulture Shuttle during ascent, showing the MK4 orbiter and side-booster configuration.</div></div></div>
|
|
<div id="vulture-img-recovery" class="wiki-modal"><div class="wiki-modal-card"><a class="modal-close" href="#">x</a><img src="/vulture/vulture_booster_recovery_original.png" alt="Vulture liquid booster recovery" data-wiki-asset="/vulture/vulture_booster_recovery_original.png"><div class="thumbcaption">Reusable liquid booster recovery after RTLS return and propulsive landing.</div></div></div>
|
|
<div id="vulture-img-separation" class="wiki-modal"><div class="wiki-modal-card"><a class="modal-close" href="#">x</a><img src="/vulture/vulture_booster_separation_original.png" alt="Vulture liquid booster separation" data-wiki-asset="/vulture/vulture_booster_separation_original.png"><div class="thumbcaption">Liquid booster separation before the orbiter and external tank continue toward suborbital insertion.</div></div></div>
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