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There's another reason the CIA and NTSB zoom climb is untenable. The Center Wing Tank they claim exploded is not merely a tank but it is a structural member of the airframe to which the wings attach. If the explosion occurred in the Center Wing Tank, the structure would have been majorly compromised and could NOT have supported the forces necessary for any climb at all.

The Center Wing Tank was recovered from the bottom of the Atlantic and does not show any signs of being "exploded" such as walls bowed outward from the force of an explosion. Instead, where the walls are damaged, they are bowed INWARD, from a force acting from the outside.

If I recall correctly, although I don't have a photo of it, the forward spar which formed the forward bulkhead of the tank, was also bowed inwards, not outward. The G forces required for the 3800 feet climb of the CIA in 18 seconds is literally beyond the stress limits of the 747 with an intact Center Wing Tank. With a compromised Center Wing Tank, it's doubtful the wings would have stayed attached, much less carried the plane aloft that distance. Absent a good attack angle to achieve lift, and given no power, that plane did not climb.

Boeing 747-100 — Note the CWT is located below where the wing escape door is located.
The nose break point is just forward of the wing, about where the "D" ends with the door below it.

The nose of the plane broke off about 20 feet forward of the Center Wing Tank. Not where any of the forces from a Center Wing Tank explosion would be anywhere

The Swordmaker Timeline of TWA-800

This timeline was based on my examination of the radar returns, both active and passive, debris fields, wreckage recovery, and the blackbox data and eye-witness reports that I deemed credible. Other Freepers critiques and inputs were considered and when suitable, resulted in changes to the timeline. This was constructed back in September 2002 in response to a Freeper named Asmodeus whose rude and reprehensible behavior toward other Freepers he disagreed with on this topic got him banned.

20:31:00 — Plane flying normally, altitude 13,400 ft., climbing at 33 ft/sec.
21:31:04 — Possible ground-to-air missile launch. Rate of climb accelerates to Mach 2.1.
20:31:07 — Mike Wire notices flare like object rising over house and arcing to left. in the next 8 seconds many more people notice streak, firework, etc.
20:31:10 — Major Fred Meyer sees "meteor like" object flash across his field of view.
20:31:12 — ~13,800 ft. - 0 sec. Last transponder return, everything normal, Aircraft climbing at 33 ft./second.
20:31:13 — ~13,840 ft. ~1 sec. Missile strikes TWA800 on left side at approximately seat row 16-17 transects the passenger cabin spewing partially burned solid rocket fuel (and leaving a red residue on seats in this area), taking out passengers and seats in rows 17-18 and exits aircraft through right side. VDR ends in loud, strange sound. Bright white Ordnance type explosion occurs just after missile exits thin walled cabin. Blast places massive overpressure on nose of aircraft and opens wide gap in side of aircraft. Parts of missile continue on momentum at speed approaching MACH 2 at a vector 190 degrees from north, ejecta from aircraft including seats, passengers, luggage to eventually land in "crosswind blast debris" field. The blast imparts a slightly more eastward vector for the ejecta which combined with the ejecta's already present eastward momentum results in the ejecta coming to rest about 175 degrees from the point of ejection.
20:31:14 — ~13,880 ft. ~2 sec. 400+ MPH winds acting on the gaping holes in aircraft fuselage causes the "unzip" of the aluminum skin of the nose. Windforce bends the nose up and breaks the "keel" of the fuselage. Signals to control surfaces and engines cease when wires are broken and engines revert to idle. Drag is no longer being counteracted by the thrust of the engines. The plane slows drastically.
20:31:15 — ~13, 900 ft - ~3 sec. Drag pulls the nose up and away from the rest of the fuselage and breaks loose on the right first and falls away to the left where it is still partially attached, twisting the aircraft toward the left and starts to fall pulling the left wing down, changing the vector of lift imparting a strong leftward force on the aircraft. Unbalanced drag toward the left is enormous. This accounts for the sudden leftward change in aircraft vector.
20:31:16:49 — ~13,890 ft - 4.49 sec. First post IE radar return. - The nose swings under and to the right and breaks completely loose and continues on a momentum driven ballistic fall slightly to the right (about 3 degrees) of the original aircraft vector. The noseless aircraft losing both the balance necessary for proper flight AND the thrust of the engines overcoming drag, pitches rapidly up and stalls. it may climb a very small amount during the pitch up before stall.
20:31:17 — ~13,860 ft. - ~5 sec. Gravity's inexorable pull starts the plane on its final trajectory. Drag is slowing the forward velocity and the uncontrolled aircraft is on either a ballistic fall or a somewhat aerodynamic fall.
20:31:21:13 — ~13,500 ft. - 9.13 sec. Second post IE radar return. - Uncontrolled plane pitches and yaws, lift occasionally pulls the plane in different vectors... this time a strong rightward vector. Drag continues to rip and rend the airframe just in front of the wing.
20:31:25:72 — ~12,300 ft. - 13.72 sec. Third post IE radar return. - More gyrations... now vectored back to the right.
20:31:30:37 — ~10,900 ft. - 18.37 sec. Fourth post IE radar return. - Falling steeply now. Much of the forward momentum is gone due to drag. Structural damage is weakening the Center Wing Tank's integrity and wings are no longer as strongly attached to the remaining fuselage.
20:31:32:?? — ~10,050 ft. - ~20 sec. Terminal velocity achieved of ~450 ft./second.
20:31:34:97 — ~9,100 ft. - 22.97 sec. Fifth post IE radar return. Stress is taking its toll on the wingroots. The Center Wing Tank structural members are buckling under the whipping of the plane rolling and pitching. Fuel is now leaking into the area around the Wing roots from the full wing tanks.
20:31:36:?? — ~8,500 ft. - ~24 sec. The aircraft takes a VERY sharp turn to the right (South) and one of the wing's fails, breaking away from the fuselage. The aircraft with only one wing starts to spin rapidly, spewing jet fuel and agitating it into the atmosphere, mixing it with air.
20:31:39:64 — ~7,000 ft. - 27.64 sec. Sixth post IE radar return. - Center Wint Tank explodes from spark caused by MECHANICAL breaking of metal. Volatile air-fuel mix surrounding aircraft ignited into Massive Fireball, Hot fireball begins to RISE, while burning plane falls through bottom of Fireball still spewing liquid fuel which ignites on exit from wing tanks.
20:31:43 — Elmer's "Streak of light" crippled plane appears.
20:31:44:29 — ~4,900 ft. - 32.29 sec. Seventh post IE radar return. - Still falling at 450 ft. per second.
20:31:47 — ~3,680 ft - End of streak - Elmer Asmodeusu's mythical "Eyewitness Myth" Explosion of Massive Fireball at 5500-7500 feet.
20:31:48:94 — ~2,800 ft. - 36.94 sec Eighth post IE radar return. - Shortly after the Flight TWA800 falls below the radar horizon and no further radar returns are received.
20:31:55 - ~43 splashdown.

Total Elapsed time from Initiating Event (the missile strike) = ~43 seconds. Plus or minus 2 seconds.