Schweizer SGS 1-34
|SGS 1-34 with terminal velocity dive brakes deployed|
|National origin||United States|
|Manufacturer||Schweizer Aircraft Corporation|
|Variants||Martin Marietta Model 845|
The 1-34 was designed over a number of years in the mid-1960s and first flew in 1969.
Design and development
The 1-34 was designed over several years to spread out the development costs. At the time the design work on the aircraft was started the Standard Class was new and described a very simple aircraft with terminal velocity dive brakes, fixed landing gear and no water ballast. By the time the 1-34 had flown in 1969 the Standard Class rules had changed to allow essentially unrestricted sailplanes with a 15-metre (49.2 feet) wingspan.
The 1-34 has the originally specified terminal velocity dive brakes, that limit the glider to below redline speeds in a vertical dive. Developing and testing these proved expensive and time-consuming and this also extended the aircraft's development time.
The 1-34 was the first Schweizer design to depart from using a NACA airfoil. The 1-34 has no wing washout and instead uses a Wortmann FX 61-163 airfoil at the wing root transitioning to a Wortmann FX 61-126 airfoil at the wing tip. The tip airfoil stalls at a higher angle of attack, ensuring that the wing root stalls first.
The one company concession to the changing Standard Class rules was the development of a retractable landing gear version of the 1-34, designated as the SGS 1-34R.
The 1-34 also features in-flight adjustable rudder pedals and a two-way adjustable seat to accommodate pilots of different heights.
During the protracted development process, Schweizer Aircraft was aware that the 1-34 would be overtaken by the changes in class rules and also by the performance of the newer European fiberglass sailplanes, but continued development of the SGS 1-34 anyway. The company identified that there was demand from private owners and especially clubs and commercial operations for a simple, rugged single seat glider with greater performance than the 1-26.
In service the 1-34 has proven to be a popular club aircraft and ideal for the completion of badge flights. If a greater number of 1-34s had been built, Schweizer indicated that it would have become another one-design class, similar to the 1-26.
At least two 1-34s have been highly modified. Bob Park's 1-34R, registered N17974, was damaged when a hurricane passed through Georgia and resulted in a hangar collapse. The 1-34R was rebuilt with a V-tail and ballast tanks mounted in the wings that hold 230 lbs (105 kg) of water. The aircraft was subsequently registered in the experimental Racing - Exhibition category.
A modified SGS 1-34 airframe with tricycle landing gear and powered by a Lycoming TIO-360 piston engine was used as the basis for the pilotless Martin Marietta Model 845 prototype, an entry in the early 1970s USAF Compass Dwell endurance UAV program.
The USAF designation for the SGS 1-34 is TG-6.
- The original fixed landing gear 1-34 model was certified under type certificate G3EA on 16 October 1969.
- The retractable gear 1-34R was added to type certificate G3EA on 15 June 1971.
- Park 1-34R Modified
- After a hangar collapsed on Bob Park's 1-34R and destroyed the aft part of the aircraft he rebuilt it in the Experimental - Racing/Exhibition category with a V-tail and 230 lb (104 kg) of water ballast. The new tail allowed 18 lb (8 kg) of lead nose ballast to be removed. The aircraft flew three diamond goal and gold distance flights in August 1983.
Aircraft on display
- Crew: One
- Length: 25 ft 5 in (7.80 m)
- Wingspan: 49 ft 3 in (15.00 m)
- Height: 7 ft 6 in (2.31 m)
- Wing area: 151 ft2 (14.0 m2)
- Aspect ratio: 16
- Wing profile: Root: Wortmann FX 61-163, Tip: Wortmann FX 61-126
- Empty weight: 570 lb (259 kg)
- Gross weight: 840 lb (381 kg)
- Maximum speed: 142 mph (227 km/h)
- Maximum glide ratio: 33 at 55 mph (88 km/h)
- Rate of sink: 144 ft/min (0.73 m/s)
Aircraft of comparable role, configuration and era
- Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 32. Soaring Society of America, November 1983. USPS 499-920
- Activate Media (2006). "SGS 1-34 Schweizer". Archived from the original on 2008-05-27. Retrieved 2008-05-25.
- Schweizer, Paul A: Wings Like Eagles, The Story of Soaring in the United States, page 241. Smithsonian Institution Press, 1988. ISBN 0-87474-828-3
- Federal Aviation Administration (September 2007). "GLIDER DATA SHEET NO. G3EA" (PDF). Retrieved 2008-05-25.
- K & L Soaring (n.d.). "K & L Soaring, LLC". Retrieved 2008-04-05.
- Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 63. Soaring Society of America, November 1983. USPS 499-920
- Federal Aviation Administration (June 2011). "Make / Model Inquiry Results N17974". Retrieved 15 June 2011.
- Designation-Systems.Net (June 2009). "Martin Marietta 845A". Retrieved 2009-06-21.
- Federal Aviation Administration (May 2008). "FAA Registry". Retrieved 2008-05-25.
- Transport Canada (May 2008). "Canadian Civil Aircraft Register". Archived from the original on 2008-05-03. Retrieved 2008-05-25.
- US Southwest Soaring Museum (2010). "Sailplanes, Hang Gliders & Motor Gliders". Retrieved 26 May 2011.
|Wikimedia Commons has media related to Schweizer SGS 1-34.|