Douglas A3D Skywarrior Entry/Exit Doors

 The Skywarrior bombers had a self-boarding arrangement* that also did double duty as a bailout slide:

It consisted of an inner (upper) and outer (lower) door. When closed, the inner door formed the bottom of the cockpit floor and sealed the crew compartment for pressurization; the outer door closed off the opening in the bottom of the fuselage. Large indentations, two in the inner door and three in the outer door, served as steps and hand grips and still allowed the doors to have a smooth surface to function as a slide for bailout.

However, the following picture of a crewman ascending into the cockpit included a feature not included in the illustration above, a rectangular transverse ledge (highlighted by question marks) with a raised non-skid pattern.

On close examination (you can see successive ledges below the top one), I finally realized that in this instance, climbing into the airplane had been made easier—particularly if you had something in your hands—by leaning a folding ladder up against the outer door.

* Skywarrior versions had similar arrangement that was different in detail, including the arrangement of steps:

Also see http://tailspintopics.blogspot.com/2013/05/trumpeter-148-a3d-forward-fuselage.html).

McDonnell F2H-2B Banshee

This post incorporates material provided from the Greater St. Louis Air and Space Museum by Mark Nankivil.

Click HERE for my previous post on the "Nuclear Banshees". When I get a chance, I'll correct some of the discrepancies in it. Click HERE for my F2H Banshee Modeler's Notes: it includes links to several of my other posts on the Banshee.

By the early 1950s, the Mk 7 and Mk 8, tactical nuclear weapons small enough to be carried by single-seat fighters and bombers, had been developed. The U.S. Navy quickly modified two carrier-based airplanes to accommodate them, the Douglas AD Skyraider (see http://tailspintopics.blogspot.com/2022/04/ad-4-skyraider-variant-ad-4b.html) and the McDonnell F2H Banshee. The suffix B was added to the designation of these airplanes to identify them as having non-standard armament.

The Mk 7 was lighter (about 1,680 lbs) than the Mk 8 (about 3,250 lbs) but much larger (30.5 inches in diameter and 182 inches long). To fit it under the inboard wing of the F2H-2 required that the landing gear shock struts be pressurized to extend them to their full travel.

The nose landing gear extension;

The extension required the addition of small hydraulic reservoirs to add fluid to and remove fluid from the shock struts as required:

The result increased the height of the requisite pylon above the ground by 10 inches, providing just enough clearance for a carrier launch with a Mk 7:

 

 

Note that the tail cone had to be installed "upside down" to provide clearance from the underside of the wing. This also meant that the retracted tail fin could not be extended before the bomb was dropped, so the electric motor that did that was replaced by first one and then two springs; the fin was held in the retracted position by a locking device until the bomb was dropped and a lanyard attached to the pylon opened it.

 

An elaborate arrangement of sway braces and a spring-activated separation device on the inboard aft end of the bomb was required to carry and safely separate the bomb from the Banshee when it was dropped.

Loading the Mk 8 did not require extending the shock structs but did require that the left inboard flap extension be disabled.

(For a dimensioned drawing of the Mk 8, see the AD-4 link above.)

It necessitated a different pylon/shackle (30-inch distance between lugs for one thing), arrangement of sway braces, and a simpler separation feature.

 

 The left inboard flap had to be locked up for clearance with the Mk 8 tail fin:

The pylon location, on the same wing station as the original inboard stores pylon, was the same for both bombs; a notch in the center section flaps was provided for Mk 7 clearance (not shown is the recess on the outboard center section flap for the Mk 8 fin clearance noted above).
 

 It was essentially coincident with the outboard edge of the engine intake opening:

Note that this initial capability predated the development of the Low Altitude Bomb System (LABS) delivery (click HERE). Instead, the bomb was to be dropped from altitude, in this example in a dive utilizing a "loft" bomb deliver capability, not to be confused with the loft options provided by LABS,

The flight manual advised caution not to exceed G limits when the Mk 7 was released in the loft maneuver; use of loft delivery for the much heavier Mk 8 was prohibited.

A couple of details on the Mk 7 development: 

Problems with its stability and trajectory were discovered during initial test drops. This was solved in part by adding wedges one one side of the tips of the tail fins that resulted in the bomb spiraling like a football.

Another was the initial use of barometric pressure to provide an air-burst capability for more wide-spread devastation. However, as the Mk 7 neared the ground, it was going faster than the measurement of the air pressure could keep up with from a detonation accuracy standpoint. As a result, speed brakes were initially provided between the tail fins that opened up when the bomb was dropped (it probably also provide a few vital seconds for the pilot to get far enough away to avoid getting "hoist by his own petard").

The addition of radar sensing of the height above ground resulted in them being deleted from the Mk 7.

Note that the Mk 8 did not required speed brakes because its raison d'etre was destruction of well-protected submarine shelters, accomplished by not detonating until as far below ground as possible.

 The development of bespoke pylons (to be described in a subsequent post covering the F2H-3/4 nuclear-strike configuration) and more options for changing the angle of the tail cone allowed the Mk 7 to be loaded with the fins pointed upwards and eliminated the separate sway braces required for the Mks 7 and 8.

An important feature of the F2H-2B was the addition of the newly developed inflight refueling capability. This was accomplished by adding a fuel probe replacing one of the 20mm cannons on the right side of the fuselage.

Only the fuselage fuel tanks could be refilled in flight, probably because these early jets did not have single-point refueling capability. Also filling the tip tanks would have required the addition of additional fuel lines and flow management valves and controls. That was a tradeoff against the extra range that would be achieved, particularly since even though the store was mounted fairly close to the center line, the tip tank on that side could only be partially filled before takeoff since only so much lateral imbalance could be offset by the roll-control power (i.e. aileron effectiveness) available at low speeds. At cruise speeds, however, the imbalance could probably be accommodated, albeit at some increase in drag due to the control-surface deflection.

The early refueling probe had a tip that resembled a baby bottle nipple. It was subsequently replaced by the one that's now standard across U.S. and NATO probes.

There is currently a discrepancy in the number of F2H-2Bs. In my earlier post on Nuclear Banshees (see link above including comments) there were 25 to as many as 31, depending on the source. The effectivity given in the 15 January 1954 document provided by Mark Nankivil lists 60!:

125030-70

125500-05

125650-62

In any event, the F2H-2Bs were deployed in both "composite" squadron detachments and fighter squadrons:

This squadron's markings in color and regrettably, a bit out of focus:

Roden 1/72 AJ-1 Savage Review

 

Model and Photo by Paul Boyer

Paul Boyer's review of the excellent Roden 1/72 scale AJ-1 kit here: Fine Scale Modeler

He mentions the windshield wiper location (note that this AJ-1 canopy has been modified with the larger escape hatch);

 

A couple of other easily fixable nits:

1. The AJ-1 had a single, rectangular (except for forward lower/right corner) nose landing gear door; the kit provides the AJ-2's two-piece door. An easy change:

2. The kit canopy represents the fix to the original sliding canopy with white fiberglass straps glued on it to strengthen it; only a few early production AJs were delivered with the version (I've not seen a picture of a Savage on a carrier with this canopy):

This was quickly replaced by a non-sliding, framed canopy:

In building the kit for review, Paul chose to simply paint the existing frames blue. However, a close approximation of the early AJ-1 canopy (note that it has a small sliding window beside both the pilot and bombardier) can be easily created by 1) sanding off the last transverse frame and the longitudinal frames fore and aft of it and 2) representing the structure on the back of the canopy with a thin layer of filler.

For more on the AJ Savage canopy variations, click HERE.

I was particularly impressed by the detail and accuracy of cockpit detail. Whoever did the research should be commended. The only minor exceptions, like some of the detail provided, will not be visible when the kit is assembled.

Kit parts 2K and 37K should provide for an opening under the flight deck to the left of the nose wheel well for access to the electronics forward (this is a photo of the AJ-2 at the National Museum of Naval Aviation):

The area aft of kit part 17E, which is the forward end of the fuselage fuel tank, should therefore be filled in to represent it accurately.

Note that there is a door/hatch in kit part 23K that was required when the nuke in the bomb bay had to be armed after takeoff. It may not be as tall as it should be since this installation shows it extending up to what is the bottom of the fuselage fuel tank...

I'm not sure that there should be an opening in kit part 15K but it's possible because 1) the jet engine firewall is aft of that and 2) the tanker installation requires a "fuel splash door" to be fitted here.

For other posts for reference for added detail, click HERE.