To name a few
- HAL Ajeet (An additional pair of hardpoints added from the original pair present on the original Folland Gnat).
- L-1011 TriStar operated by Orbital Sciences (A centerline pylon has ben installed to allow the aircraft to carry a space launch vehicle),
- LiM-5 (I don't know if it counts as modern .... an additional pair of hardpoints was added at the wing roots from the original MiG-15/17 design).
- Boeing 707 converted to tankers
- Airbus A330 tanker
- P-2 Neptunes retrofitted with underwing turbojets.
- CASA C-212 Aviocar maritime patrol variant
- EMBRAER EMB-110 Bandierante maritime variant (I believe it is designated P-95 in Brazilian service).
- Gulfstream G-IV EW variant
I agree with you in that retrofitting weapon pylons on aircraft is not an easy task, but it can (and has) been done. Obviously, the ease (and expense) of making such modifications will be a factor while selecting the aircraft.
Its not impossible just difficult, especially with transport aircraft.
Lets have a look at any special features in the manner in which it was achieved in the examples provided.
HAL Ajeet – The wing was essentially redesigned internally and built with new outer wings with additional sub-spars.
L-1011 – Centerline pylons are usually easier than wing pylons.
LiM-5 – Again with fighters its easier, the closer to the centreline the better.
Boeing 707 converted to tankers – well strictly it was the other way around, the KC-135 (and its prototype predecessors came first).
Airbus A330 tanker – Interesting that the same wing was used for the A340 and the refuelling pods are mounted on the hard points for the additional two engines.
P-2 Neptunes – An older aircraft with greater margins than modern aircraft, but again I think that the basic structure was in place and was adapted to mount the additional engines. (The same storey for the B-36 Peacemaker)
CASA C-212 – Most aircraft I have seen with additional hard points have been equipped with small external fuel tanks 250 – 500l I would estimate.
Embraer EMB-110 Bandierante – With a straight wing the some of the military versions have hard point for relatively light loads. I think that the wing was heavily modified to take the tip tanks at the same time (essentially a new wing).
Gulfstream G-IV EW variant – I know a bit more about this one. Again the work was carried out from new and was a little easier because the rear fuselage engine mounting simplified the structure of the wing.
Boeing 747 – Some aircraft have been manufactured with a hard point outboard of the engines in order to carry a spare engine to an airfield where it is required by another aircraft. I think that this technique was also used on other B707 style aircraft. I don’t think this is done so often these days, with the improved reliability of aircraft engines and the availability of large capacity cargo aircraft.
As we can see from the above, there are three approaches to getting hard points on an aircraft.
1 The basic provision for provided in the original aircraft and has been adapted. (i.e. hard points for weapons used for engines).
2 The structure of the aircraft was easily to modify, straight wings, traditional rib, stringer and spar construction. There are two locations where strong points are already included in many aircraft. Jacking points and the strengthened rib where in wing inner panels join to the outer panel. In early designs this was a convenient place to divide the wing making for easier transport and also because the outer panel was often a slightly different aerofoil (preventing tip stall) and carrying less load could be made of lighter materials.
3 It has to be a specific aircraft and so a new wing must be developed.
With smaller transport aircraft adapted to carry external stores it is usually not the total payload that is the limiting factor in determining the maximum mass of weapons that can be carried, but rather the distribution of the point loads and the manner in which these loads are spread within the structure of the wing.
When aircraft are originally designed part of the specification describes the typical loads that the aircraft will experience in different phases of the flight. For transport aircraft this would mainly be, taxing, take-off, climb, cruise descend, land, ground-run and back to taxing. Obviously for military aircraft combat scenarios also have to be included. Each area of the aircraft is assigned an estimate of the vibration (acceleration), shock loads and that are likely to experienced in that area. Similar estimates are provided for temperature, acoustic noise and in the case of external areas aerodynamic loads. In additional all regions have specifications for resistance to corrosion to the environment to which they will be exposed. A combination of the time the aircraft is anticipated to spend in each aspect of the flight and the number of load cycles experienced (usually take of and landing, but can include hi-g manoeuvres for combat air and de-pressurisation for commercial aircraft) is used to determine the planned life of the aircraft.
Adapted aircraft impose additional loads on the aircraft that were not in the original design. With heavy external loads, the mechanical aspects of the specification are important. When designing a hard point we need to consider not only the mass of the weapon but the typical shock loads that can be experienced. An emergency landing just after take-off with a full load fuel and bombs on a rough strip is an extreme example of what the weapons stations must be able to withstand. Trapped carrier landings are another example, but are rarely attempted by anything other that an aircraft designed from the outset for this purpose.
Because adapted aircraft are operated in a different manner than originally intended, such aircraft often have a reduced fatigue life and/or have to undergo additional maintenance and modification.
So in summary, incorporating hard points in the wings of turboprop powered aircraft is possible but often difficult. It requires a great deal of detailed investigation to determine if the propositions are practical or even possible. For some aircraft it will be easy, with others almost impossible. In most cases in is difficult to tell which aircraft will be in which category without a detailed investigation.
With modern PGMs external carriage may not be necessary, particularly with the latest range of small smart weapons.
With a little lateral thinking a multi-tier approach could offer a cost effective approach to COIN operations.
In remote areas it is extremely difficult to eliminate the activities or insurgents completely, instead the main objects are to contain and suppress the level of activity to an acceptable level.
A well thought strategy with the right platforms, weapons and sensors, could result in an effective system that would deter the opposition, whilst rarely having to drop live weapons.
Chris