Fix technical inaccuracies identified in PR review
· 7 months ago
f738781f4112beed3a492f5d7ed21b6652dfe3fd
Parent:
a64eab696
Engine specifications:
- Vulcan Centaur: Corrected from '2 RS-25 + BE-4' to '2 BE-4'
- Long March 5: Updated to '2 YF-77 (core) + 4 YF-100 (boosters)'
- Angara A5: Corrected engine count from 6 to 5 RD-191 (1 core + 4 boosters)
Thrust values:
- Long March 5: Updated from ~1,220 kN to ~6,280 kN (~1,410k lbf)
- Vulcan Centaur: Corrected from ~2,400 kN to ~4,800 kN (~1,078k lbf)
- Ariane 6: Clarified thrust notation to '~1,350 kN (core) + ~18,000 kN (boosters)'
Mass data:
- New Glenn: Reverted unverified estimate to 'N/A'
- Vulcan Centaur: Reverted unverified estimate to 'N/A'
Other improvements:
- Clarified Starship GTO payload with refueling requirement note
- Fixed Falcon Heavy description grammar ("Most of the" → "The")
All changes align with official specifications and PR feedback.
1 file changed +13 −13
- orbital-rockets-comparison.html +13 −13
Diff
--- a/orbital-rockets-comparison.html +++ b/orbital-rockets-comparison.html @@ -487,12 +487,12 @@ <tr> <th scope="row"><i class="bi bi-weight"></i> Mass (Liftoff)</th> <td>~5.3M kg (11.7M lb)</td> - <td>~1.6M kg (est.)</td> + <td>N/A</td> <td>773k kg (1.7M lb)</td> <td>~860k kg (1.9M lb)</td> <td>1.42M kg (3.13M lb)</td> <td>643k kg (1.4M lb)</td> - <td>~1.9M kg (est.)</td> + <td>N/A</td> <td>549k kg (1.2M lb)</td> </tr> @@ -504,11 +504,11 @@ <th scope="row"><i class="bi bi-gear"></i> First Stage Engines</th> <td>33 Raptors</td> <td>7 BE-4</td> - <td>6 RD-191</td> + <td>5 RD-191 (1 core + 4 boosters)</td> <td>4 Vulcain 2.1 + 2 Solid</td> <td>9 Merlin (cores)</td> - <td>2 YF-100</td> - <td>2 RS-25 (SSME)</td> + <td>2 YF-77 (core) + 4 YF-100 (boosters)</td> + <td>2 BE-4</td> <td>9 Merlin</td> </tr> <tr> @@ -516,10 +516,10 @@ <td>~76.7 MN (~17.2M lbf)</td> <td>~1,900 kN (~427k lbf)</td> <td>~2,090 kN (~470k lbf)</td> - <td>~6,200 kN + Solid</td> + <td>~1,350 kN (core) + ~18,000 kN (boosters)</td> <td>~7,590 kN (3 cores)</td> - <td>~1,220 kN (~274k lbf)</td> - <td>~2,400 kN (est.)</td> + <td>~6,280 kN (~1,410k lbf)</td> + <td>~4,800 kN (~1,078k lbf)</td> <td>~690 kN (~155k lbf)</td> </tr> @@ -540,7 +540,7 @@ </tr> <tr> <th scope="row"><i class="bi bi-geo"></i> Payload to GTO</th> - <td>~53,000 kg (est.)</td> + <td>~53,000 kg (with in-orbit refueling)</td> <td>13,600 kg</td> <td>5,400 kg</td> <td>11,500 kg (A64)</td> @@ -719,7 +719,7 @@ <span class="stat-label">First Flight:</span> <span>Feb 6, 2018</span> </div> - <p style="font-size: 0.95rem; margin-top: 1rem; color: #ccc;">Composite of three Falcon 9 first stages clustered together. Most of the highest-capacity operational rocket, with proven reusable booster landings.</p> + <p style="font-size: 0.95rem; margin-top: 1rem; color: #ccc;">Composite of three Falcon 9 first stages clustered together. The highest-capacity operational rocket with proven reusable booster landings.</p> <div class="rocket-links"> <a href="https://www.spacex.com/vehicles/falcon-heavy/" target="_blank" rel="noopener"><i class="bi bi-globe"></i> Official Site</a> <a href="https://en.wikipedia.org/wiki/Falcon_Heavy" target="_blank" rel="noopener"><i class="bi bi-wikipedia"></i> Wikipedia</a> @@ -844,7 +844,7 @@ <div class="stat-row"> <i class="bi bi-fire"></i> <span class="stat-label">Engines:</span> - <span>2 RS-25 + BE-4</span> + <span>2 BE-4</span> </div> <div class="stat-row"> <i class="bi bi-calendar-check"></i> @@ -888,7 +888,7 @@ <div class="stat-row"> <i class="bi bi-fire"></i> <span class="stat-label">Engines:</span> - <span>6 RD-191</span> + <span>5 RD-191 (1 core + 4 boosters)</span> </div> <div class="stat-row"> <i class="bi bi-calendar-check"></i> @@ -931,7 +931,7 @@ <div class="stat-row"> <i class="bi bi-fire"></i> <span class="stat-label">Engines:</span> - <span>2 YF-100</span> + <span>2 YF-77 (core) + 4 YF-100 (boosters)</span> </div> <div class="stat-row"> <i class="bi bi-calendar-check"></i>