Meillerwagen Manufacturer Gollnow & Son Assembly Germany Class trailer Wheelbase 9,800 millimetres (32.2 ft) Length 14,700 millimetres (48.2 ft) Width 2,800 millimetres (9.2 ft) Height 3,270 millimetres (10.73 ft) Curb weight 11,300 kilograms (25,000 lb) Related SdKfz, Vidalwagen
The Meillerwagen (English: Meiller Vehicle) was a German World War II trailer used to transport a V-2 rocket from the 'transloading point'1 of the Technical Troop Area to the 'launching point', to erect the missile on the Brennstand (English: firing stand),2 and to act as the service gantry for fuelling and launch preparation. The unofficial 'Meillerwagen'3 name was often used in official documents and refers to a parts supplier for the trailer, Meiller-Kipper GmbH of Munich, Germany (founded 1850). The Army Research Center Peenemünde designed the Meillerwagen, and the Gollnow & Son company assembled the Meillerwagen from supplied components. The Meillerwagen was assembled with Italian and Russian prisoner laborers of the Lager Rebstock. The Meillerwagen was vehicle code number 102 of several vehicles in a V-2 launching battery, which included an 8 ton launch control vehicle. Launching of V-2s from mobile equipment was studied under code name Regenwurm ("Earthworm") to replace bunkers such as at the Watten bunker.
External media Launch vehicles
The Meillerwagen A-4/V-2 transport-launcher device as conformed by next vehicles:
- Feuerleitzugmaschine Sd.Kfz. 7/3 (command vehicle)
- Feuerleitpanzer Sd.Kfz.251 (command vehicle)
- Hanomag SS-100 (tractor vehicle)
- Meiler-Wagen (V-2 mobile wagon-launcher)
- Opel-Blitz T-Stoffwagen (fuel car-tanker)
- Kesselanhänger für Fl-Sauerstoff (liquid oxygen wagon-tanker)
After completing the process of fitting the warhead to the V-2 rocket, the Technical Troop used a strabo crane at the transloading point to transfer the missile from the Vidalwagen to the Meillerwagen for transport to the launching point. Typically a Hanomag SS-100 tractor pulled the Meillerwagen up to 45 km/h (28 mph) forward with the rocket travelling tail-first – the maximum speed in reverse was 15 km/h since the Meillerwagen's pneumatic brakes could not be coupled to the tractor when being pulled backward.
After the Meillerwagen was close to the launch point, the Firing Platoon Truck Section took charge and removed the rocket's camouflage cover and rudder protection. The control compartment batteries, alcohol-filling connection, tools, and other equipment were loaded into a box on a strut at the top of the Meillerwagen's lift frame. The Meillerwagen was moved via hand winches to the firing stand and then levelled via the two extendable outriggers with end-jacks.
The rocket was raised via the Meillerwagen lift frame and hydraulics. When vertical, the rocket was suspended above the firing stand, which was raised to touch the rocket fins. Clamping collars were used to connect the rocket to the firing stand, and the Meillerwagen was withdrawn less than a meter and the rocket was turned a quarter turn for the fuel connections to face the Meillerwagen platforms, which were lowered into position for standing. A separate three-section extendable ladder, the Magirus ladder, was used for areas of an erected rocket not accessible via the Meillerwagen.
The hydrogen peroxide tank on the Meillerwagen (126 litres) was filled from a 2120-litre tank truck with its own pump, then the rocket was filled from the Meillerwagen tank. Additionally Meillerwagen piping included the following:
- Fuel Pipes
- The elevated lifting frame was fitted with piping to fuel the rocket with A, B, P, and T-stoff.
- A-stoff: Liquid oxygen equipment consists of a pipe, which follows a circuitous route along the centreline of the lifting frame’s lower half. The pipe is fixed on the lifting frame by brackets, and closed at each end by cast ramp-and-claw seals.
- B-stoff: Ethyl alcohol equipment consists of a pipe which runs along the full length of the starboard beam of the lifting frame. The pipe is slung from the underside on straps, and closed at each end by threaded seals.
- P-stoff: Compressed nitrogen (or compressed air) equipment to service the rocket consists of several batteries of compressed air tanks carried on the chassis frame, and a pipe fixed to the full length of the starboard beam of the lifting frame. The P-stoff batteries consist of one bank of six fixed tanks, and two banks of two removable tanks. (compressed air for the Meillerwagen pneumatic brakes was sourced from a separate set of two tanks across the front of the chassis frame)
- T-stoff: Hydrogen peroxide equipment consists of a pipe which runs along the starboard beam of the lifting frame from the trunnion end to the halfway point. The pipe is fitted at the upper end to the triple valve assembly, consisting of two flow valves and a three-way valve. The triple valve assembly connects to two tanks, a large measuring tank and a smaller overflow tank. The measuring tank can be filled to the rocket's required amount of T-stoff, after which any excess flows down a stand pipe to the overflow tank. The measuring tank is fitted with a ventilation stud, which vents displaced air as the tank is filled. The ventilation stud includes a ball cock fixed to a frustum stopper, which blocks the vent stud in case of accidental overfilling so that T-stoff does not spray from the air vent. Both T-stoff tanks are fitted with an inspection window.
The structure of the Meillerwagen consisted of the wheeled trailer chassis, and the hydraulic lifting frame.
The trailer chassis was a lattice frame of tubular members. It comprised a transverse trunnion box member at the front, from which six longitudinal tube members ran aftward and converged into one large main central tube at the rear; the six longitudinal members were braced vertically and horizontally by smaller-gauge tubes. The rear central tube member supported a large horizontal-plane turntable. A steerable front truck was installed just behind the trunnion box member, while the turntable surmounted a two-axle rear bogey.
The steerable front truck was fitted with twin duplex wheels (four tyres), the inner wheels equipped with pneumatic drum brakes. The duplex wheels rode on swinging wishbone axles with transverse semi-elliptical leaf spring suspension. A steering lock was included for use during rear towing.
A turntable at the rear of the chassis frame supported a bogey, mounted on bearings so it could swivel and pivot. The bogey was fitted with two axles, a fixed middle axle and a steerable rear axle, both of the swinging wishbone type with transverse semi-elliptical leaf spring suspension. The middle axle was fitted with pneumatic brakes, while the rear axle was unbraked. A feedback steering system was included in the design, so that any change in direction by the rear bogey (and fixed middle axle) was duplicated by the steerable rear axle, but to twice the extent. The linkage for the feedback system was for used front towing, and was disengaged during rear towing.
The towing arm could be fitted to the front truck, or the steerable rear axle of the rear bogey. The towing arm was fitted with a sprung force stem, contrived so that the tow arm 'floated' horizontally at zero relative weight.
Each front corner of the chassis was fitted with a swing-out A-frame boom equipped with a screw jack and foot plate. The booms enlarged the Meillerwagen footprint to stabilise it during erection of the rocket, and provided a means of adjusting the Meillerwagen transverse level. The booms deployed outward and forward of the lifting frame trunnion axis to prevent it toppling forward or to either side.
The lifting frame was constructed of two formed I-beams, with tubular and box transverse braces. The lifting frame was fitted with plumbing for fuelling the rocket; wiring for powering and monitoring the rocket and for field telephones; accommodations for carrying and dismounting the rocket; and folding platforms to service the rocket with rungs to access them.
The lifting frame was fitted with outlet sockets and wiring for field telephones. A main connection from the armoured launch vehicle switchboard to inlet sockets on the lifting frame provided circuits for four field-phone stations at the Meillerwagen – one each at the upper and lower folding work platforms and two at the launch table.
An early configuration of the Meillerwagen included hardwiring of two electrical power circuits and two FLAK-plug circuits for the power and control needs of the rocket. The system included four sockets at the upper and at the lower end of the lifting frame, and the connective wiring fixed along the starboard beam. The four circuits were connected to two Stotz ejecting plugs, stowed with their cables along the side of the lifting frame. All of this wiring had become redundant by the time the rocket attacks began, but was not removed from the Meillerwagen.
The Meillerwagen chassis was fitted with a Notek tail light at the rear, its patch plug at the front, and the connective wiring in a conduit along the chassis frame.
The lifting frame erected the rocket from horizontal to vertical, using hydraulic power. The hydraulic lifting equipment consisted of a hydraulic pump and its drive motor, an oil reservoir tank, a control valve group with manometers, and the lifting pistons themselves. The drive motor was a petrol KdF (Volkswagen) 14 ps (hp) motor, adapted for stationary industrial use by the fitting of magneto ignition and a centrifugal governor as throttle; besides these modifications, the motor was otherwise identical to those found in VW Beetles, an air-cooled flat-four boxer. The motor was housed in a metal box fixed to the chassis frame. A three-piston eccentric-cam hydraulic pump was coupled to the drive motor flywheel. (Meillerwagens at Operation Backfire were fitted with electric motors as hydraulic drive in place of the petrol motor.)
A 70-litre (15 gal) oil tank was fixed to the chassis frame as hydraulic fluid reservoir.
Oil under pressure flowed from the hydraulic pump to the control valve group consisting of three valves in a common housing, manipulated via one large cross-handle and two small hand taps. The large cross-handle regulated the speed of raising or lowering the lifting frame. One hand tap selected direction to either raise or lower the lifting frame. The second hand tap controlled oil flow to the lowering piston (see below), to begin lowering of the lifting frame from its vertical position.
The two hydraulic lifting pistons each consisted of one stationary cylinder and four extending cylinders. The largest extending cylinder included a flange halfway along its length, against which hydraulic pressure could be selectively applied from either above or below; it was used during raising to delay its extension until all other cylinders had extended, and also to begin the lowering process when the lifting frame was vertical (once lowering had thus been initiated, gravity finished the job).
All components of the hydraulic system were products of Meiller-Kipper GmbH, except the KdF drive motor from Volkswagen.
Acting as gantry, the lifting frame included a number of work platforms from which crewmen serviced the rocket. Three (later two) platforms folded flat against the lifting frame, and could be folded out from the elevated lifting frame with the use of a hand winch. Each folding platform included a safety rail of folding posts and chains.
Two side platforms or catwalks were inserted into holders for deployment on each side of the lifting frame, otherwise stowed together on brackets near the turntable. A rotating platform could be suspended from the rocket nose, to provide access to the rocket control compartments on the far side of the rocket.
The port beam of the lifting frame was fitted with around 40 rungs along its full length, with which crewmen climbed to the working platforms.
The lifting frame included two accommodations for the rocket, a nose clamp around the warhead and a pivoting clamp around the rocket midsection. Both accommodations included a saddle, and various mechanisms to assist dismount of the rocket onto its launch table. The mechanisms were operated with two drive shafts running up the port lifting frame beam. The drive shafts ran within the integral rungs, and were operated by a crewman with a ratchet hand tool. The two drive shafts comprised a short shaft and a long shaft; both starting at the trunnion end of the lifting frame, one running half the length of the lifting frame while the other ran the full length.
The short drive shaft operated the pivot clamp around the rocket mid section, which could move the rocket 28 mm (~1") forward or backward along its centreline. The rocket midsection was fitted with a band which included trunnion pins placed in opposition; the pivot clamp held the rocket by the trunnion pins. The pivot clamp was able to rock on a transverse shaft, thus causing the rocket to move along its centreline. After erection of the rocket to a vertical position, it was held suspended above the launch table; by use of the pivot clamp, the weight of the rocket could be gently lowered onto the launch table until fully taken up, allowing the rocket to be unsecured from the lifting frame, thus dismounting it from the Meillerwagen. The short drive shaft operated a screw sleeve, which extended to work a bell crank. The bell crank turned a transverse shaft fitted with an eccentric cam, which would push or pull the pivot clamp, thus moving the rocket forward or aftward along its centreline.
The long drive shaft ran along the full length of the port beam of the lifting frame. It entered a worm gear at the pivot clamp, then continued to the nose clamp where it entered another worm gear. A shift lever at the nose clamp disengaged the drive shaft to allow either simultaneous or independent operation of the two worm gears. The worm gear at the pivot clamp operated a pair of scissor arms, one on each side of the lifting frame to insert or extract the trunnion pins from the rocket. The worm gear at the nose clamp operated the jaws of the nose clamp to either open or close, thus enclosing or releasing the rocket.
The Meillerwagen was equipped with pneumatic drum brakes, installed on the front and middle axles. The middle axle brakes could also be applied mechanically with a hand-operated cable, to act as a parking brake.
The Meillerwagen’s pneumatic brakes drew air pressure from the towing vehicle, and were operated by the tractor driver as an extension of his vehicle’s brake circuit. A control valve handle on the Meillerwagen regulated the braking force it drew from the tractor, depending on whether the Meillerwagen was laden with a rocket or unladen.
The Meillerwagen was equipped with two compressed air reservoirs, filled from the towing vehicle. These allowed the Meillerwagen to use its pneumatic brakes when it was unhitched from the tractor. In the unhitched mode, the Meillerwagen brakes were operated from the control valve handle, to provide braking ability during winching and hand-manoeuvring around the launch site.
The brake control and regulator system were supplied by Graubremse GmbH. The compressed air reservoirs, pneumatic brake cylinders and drum brakes were supplied by Knorr Bremse GmbH.
The Meillerwagen carried a number of accessories on the chassis and lifting frame, both for itself and the rocket. A toolbox fixed on the chassis carried snow chains, a tyre pump, and assorted tools for the Meillerwagen and KdF motor. The chassis was equipped with a pair of blast shields, entrenching tools, a hand-steering A-frame, two jacks, a spare tyre and a folding ladder. Special trays were fixed on the chassis to carry the transport cases which held various rocket accessories such as the graphite steering vanes, the nose fuse, and the Z-stoff (permanganate) flask. The rocket was provided with ejecting umbilical connectors, although their precise deployment evolved. Initially these 'Stotz plugs' travelled as Meillerwagen accessories, stowed on the lifting frame along with their cables. Later, the Stotz plugs were stowed in the cable box, and a ten metre cable mast was stowed on the lifting frame for ultimate erection on the launch table at the launch site.
'Laden' refers to carriage of an unfuelled rocket with warhead fitted. 'Camouflage frame' is a tube-frame box assembled around the rocket and covered with tarps, rarely used during combat launches.
- Total length: With towing arm – Unladen without Camouflage frame, 14700 mm; Laden with Camouflage frame, 16665 mm. Without towing arm – Unladen without Camouflage frame, 12610 mm.
- Shipping class: S (for the unladen vehicle)
- Total width: Unladen without camouflage frame, 2800 mm. Laden with camouflage frame, 2870 mm.
- Total height: Unladen without camouflage frame, 3270 mm. Laden with camouflage frame, 4200 mm.
- Total weight: Laden, 15476 kg. Unladen, 11300 kg.
- Axle loads: Front axle – laden, 7010 kg; unladen, 5860 kg. Middle and rear axle – laden, 4385 kg; unladen, 2720 kg.
- Turning circle radius: 10700 mm. Clearance: 350 mm.
- Maximum towing speed: forwards, 45 km/h; backwards, 15 km/h.
- Brakes: Type – Knorr single-acting pneumatic cylinders and internal-shoe drums.
- Front axle wheels: Brake cylinders, 125/140 mm; drum brake shoes, 400 x 140 mm; Pneumatic. Middle axle wheels: Brake cylinders, 80/110 mm; drum brake shoes, 400 x 120 mm; Pneumatic or cable. Pneumatic brake lines: Steel pipes, 15 mm, diam x 1.5 mm; rubber hose lines, 24.5 mm, diam x 1.3 mm. Pneumatic storage: two tanks, each of 40 litres capacity at 6 kg per cm2.
- Wheels: Type – split rim. Rim size: 8" x 20.
- Tyres: Type – Pneumatic tyres, front axle duplex tyres, middle and rear axle single tyres. Size, 270-20. Air pressure – Front axle, 4,8 atm.; Middle and rear axle, 5,8 atm.
- Wheelbase: Overall, 9800 mm; trailing rear truck, 2600 mm. Track width: Front axle, 1250 mm (central distance between duplex tyres); middle and rear axle, 2000 mm.
- Hose connectors: B-material line – steel tube of 70 mm ID; upper and lower connectors, M 90 x 2 mm; tank drain valve, M 45 x 1.5 mm. T-material line – aluminium pipe of 32 mm ID; upper and lower connectors, R 1 3/4. A-material line – light alloy pipe of 70 mm ID; Upper and lower connectors claw clutch size, NW 70 mm. P-material line – steel tube of 10 mm; 6 compressed gas bottles, 230 atm.; filling pressure with a volume of 58 L each; filling and emptying connecting pieces, AM 14 x 1,5 mm.
- Hydraulic lifting system:
- Oil pump: Design – Meiller-Kipper single-action three-piston high-pressure pump. Reservoir capacity, 70 litres; acid-free spindle oil.
- Drive engine: Design – Stationary KdF engine (from Volkswagen) type 120/15. Working type – Four-stroke petrol Otto engine. Fuel – 74 oct gasoline; Coldstart fuel, ether. Stroke, 64 mm. Bore, 75 mm. Number of cylinders, 4. Capacity, 1131 cm³. Compression ratio, 1:5,8. Working number of revolutions, 1470–1500 rpm. Continuous operation, 14 hp. Fuel consumption under full load, ~5.4 L/hr. Lubricating oil consumption, about 20 cm³/hr.
- Tools for the VW Motor: 1 starting crank, coldstart fuel (ether) in canister.
- Hydraulic presses: Number, 2. Design – 1 cylinder + 4 extending pistons (3 pressure pistons and 1 combined pressure and lowering piston).
- Accessories: hand steering pole, 2 blast shields, Stotz plugs and cables, catching net for the Stotz plugs, entrenching tools (1 pick, 1 spade), tool hoist, camouflage frame and tarps, 2 jacks, 2 side platforms. Cable Mast.
- Toolbox with contents: Cable kit, 1 Wheel-brace, 4 Snow chains, 2 Tubular extensions (for boom cranks), 2 ratchet keys (for drive shafts), Tommy bar (for frame brace turnbuckles), 1 spirit level, 1 x 4 m patch cable (for tail light), 1 crank handle (for platform winch), repair kit for catching net, Tool kit.
- Tool kit: 1 Hand pump with hose, 1 Combination pliers, 1 Mechanics hammer, 2 Tyre levers.
Of a reported production run of 200 units, three are confirmed survivors.
Australian War Memorial. Treloar Center. Canberra, Australia. (Operation Backfire emeritus, unrestored, serno 5628)
Cosford RAF Museum, Cosford UK. (Operation Backfire emeritus, restored, serno unrecorded)
USAF Museum, Wright/Paterson AFB, Ohio, USA. (A4b experimental unit, restored, serno 7364)
Unknown number taken east in 1945, all or none of which may still exist in former USSR. 
References and notes
- ^1 Terms in single quotation marks indicate Kennedy's terminology.
- ^2 A Bodenplatte (English: bottom plate) blast deflector shaped somewhat like a lemon juicer was used under the firing table.
- ^3 Many historical documents use the spelling 'Meilerwagen', but this has never been correct.
- ^ a b c d e Kennedy, Gregory P. (1983). Vengeance Weapon 2: The V-2 Guided Missile. Washington DC: Smithsonian Institution Press. pp. 44,45,48.
- ^ a b c Klee, Ernst; Merk, Otto (1963, English translation 1965). The Birth of the Missile:The Secrets of Peenemünde'. Hamburg: Gerhard Stalling Verlag. p. TBD.
- ^ Huzel, Dieter K (1960). Peenemünde to Canaveral. Englewood Cliffs NJ: Prentice Hall. p. 93.
- ^ 
V-1 · V-2 · V-3 V-1 V-2 Construction & bunkers Allied Countermeasures Related weapons Post-WWII developmentUSAOther In fiction
Wikimedia Foundation. 2010.
Look at other dictionaries:
A4 (Rakete) — Peenemünde, V2 beim Start, 1943 Aggregat 4 (A4) war die Typenbezeichnung der ersten voll funktionsfähigen Großrakete. Bekannt wurde diese Boden Boden Rakete unter dem ihr von Joseph Goebbels im Oktober 1944 gegebenen Propagandanamen… … Deutsch Wikipedia
V-2 — Peenemünde, V2 beim Start, 1943 Aggregat 4 (A4) war die Typenbezeichnung der ersten voll funktionsfähigen Großrakete. Bekannt wurde diese Boden Boden Rakete unter dem ihr von Joseph Goebbels im Oktober 1944 gegebenen Propagandanamen… … Deutsch Wikipedia
V2-Rakete — Peenemünde, V2 beim Start, 1943 Aggregat 4 (A4) war die Typenbezeichnung der ersten voll funktionsfähigen Großrakete. Bekannt wurde diese Boden Boden Rakete unter dem ihr von Joseph Goebbels im Oktober 1944 gegebenen Propagandanamen… … Deutsch Wikipedia
V 2 — Peenemünde, V2 beim Start, 1943 Aggregat 4 (A4) war die Typenbezeichnung der ersten voll funktionsfähigen Großrakete. Bekannt wurde diese Boden Boden Rakete unter dem ihr von Joseph Goebbels im Oktober 1944 gegebenen Propagandanamen… … Deutsch Wikipedia
Vergeltungswaffe 2 — Peenemünde, V2 beim Start, 1943 Aggregat 4 (A4) war die Typenbezeichnung der ersten voll funktionsfähigen Großrakete. Bekannt wurde diese Boden Boden Rakete unter dem ihr von Joseph Goebbels im Oktober 1944 gegebenen Propagandanamen… … Deutsch Wikipedia
Complexe militaro-industriel allemand — Le complexe militaro industriel allemand fonctionna à plein pendant les deux guerres mondiales. De forme évolutive, il passe des Konzern associés aux marchands de canons et d obus de la Ruhr en 1914, forme prise par le capitalisme bourgeois lié à … Wikipédia en Français
Cohete V2 — Para el artículo sobre V1, la velocidad de decisión, véase velocidades características. Cohete A4 V2 Lanzamiento de un V2 en 1943 … Wikipedia Español
Rocket — This article is about vehicles powered by rocket engines. For other uses, see Rocket (disambiguation). A Soyuz U, at Baikonur Site 1/5 A rocket is a missile, spacecraft, aircraft or other vehicle which obtains thrust from a rocket engi … Wikipedia
V-1 flying bomb — Buzzbomb redirects here. For the song by the Dead Kennedys, see Buzzbomb (song). For other uses, see V1 (disambiguation). V 1 flying bomb Fieseler Fi 103 Flakzielgerät 76 (FZG 76) V 1 flying bomb … Wikipedia
Spaceport — For the tourist attraction, see Spaceport (Seacombe). The Baikonur Cosmodrome (Gagarin s Start launch pad) A spaceport or cosmodrome (Russian: космодром) is a site for launching (or receiving) spacecraft, by analogy with seaport for ships or… … Wikipedia