Rockwell, Rockwell International
SEE ALSO Aero Commander, North American
Rockwell bought up Snow and Call-Air and consolidated operations in Albany GA, and Fred Ayers was their top dealer. At one point, Rockwell sold off the Call-Air designs to a company in Mexico. When Rockwell got out of General Aviation, Ayers bought up the Albany Division and still builds the Thrush, originally designed by Leland Snow, but developed into new models. ( David Lednicer 7/6/99)
B-1 Lancer - Intercontinental strategic bomber. 4pClwM rg; four 30780# F101-GE-102 turbofans; span: (open) 136'9" (swept) 78'3" length: 147'0" (?>143'4") v: subsonic to supersonic (M2.2/M.85/x) range: 6000+. Gross wt: 380,000#, max wt: 477,000#. Stealth-type technology, variable wings. Program cancelled June 1977, then revived Oct 1981.
Rockwell-North American B-1A (USAF Museum)
C-130U 1990 = Conversion of new Lockheed C-130Hs as close air support gunship. 13pChwM rg; four Allison T56-A-15 turboprops; span: 132'7" length: 97'9". Armed with fire-controlled 25mm, 40mm, and 105mm guns. POP: 12 as AC-130U.
Commander 111, 112A 1972 = Evolution of Aero Commander/Gulfstream Commadner. 4pClwM; two 200hp Lycoming IO-360C; span: 32'9" (?>;32'11") length: 24'11" load: 956# v: 171/161/62 (?>150/142/x) range: 975 (?>1010-1180) ceiling: 13,900; ff (111): 9/11/71 (112 with 180HP O-360-A1G6); 12/4/70. Model 111 with constant-speed prop.
Courser Commander 19?? =
North American-Rockwell Commander 114 [N5858N] (Rockwell)
Commander 114 1976 = 260hp Lycoming IO-540-T4B5D; load: 1235# v: x/157/x. $33,000; POP: ??.
Rockwell Commander 212 (Avn Week via Ron Dupas)
Commander 212 1970 = 2pClwM rg; 180hp Lycoming 0-360-AID; v: 170 range: 1200; ff: 12/4/71.
Rockwell XFV-12A (USN)
Rockwell XFV-12A (Rockwell)
FV-12 1977 = USN supersonic V/STOL fighter with 16000# P&W YF401-PW-400; span: 28'6" length: 43'11" v (projected): Mach 2+. Empty wt: 16550#. For economy, 35% of its structure came from existing aircraft (A-4, F-4, et al). Its unique Thrust Augmented Wing device was designed to run ducted air to a full-span ejector flap system in the wings and the canard ducting system to create boundary layer control similar to the blown-flap design of RA-5C. USN contract awarded in 1972. POP: 1 prototype as XFV-12A did not fly beyond hover testing at NASA.
A development contract was awarded to the Columbus Aircraft Div of Rockwell Intl. V/STOL capability was to be achieved by thrust augmentation similar to that used by the Lockheed XV-4B. Engine airflow was ducted to the canard and wings. Full-scale hover-rig tests at NASA Langley in 1978 showed that insufficient thrust augmentation was obtained. This resulted in the configuration having a thrust-to-weight ratio less than 1.0 in vertical flight mode, meaning VTOL was impossible. The contractor proposed flying the prototype from the plant to NASA Langley in VA, but that was rejected by the Navy and the program was canceled in 1981. After sitting at NASA for many years, the prototype was finally scrapped. ( Bill Blake 7/21/00)
Jetprop Commander - Turbopowered evolution of Commander with winglets, redesigned engine nacelles.
840 198? = Panorama cabin windows.
North American-Rockwell OV-10 (USN)
OV-10 Bronco SEE North American
Rockwell-North American T-2C  (USN)
T-2 Buckeye 1958 = USN/USMC carrier-capable intermediate jet trainer. 2pClwM rg; two GE 085-GE-4 turbojets; span: 38'2" length: 38'8" load: 5065# v: 520 range: 910 ceiling: 44,400'; ff (North American prototype):1/x/58 (T-2C) 4/x/68. Ejection seats. Originally designed for a single engine, it used the same wing as FJ-1. POP: ?? as T-2C, replaced by T-45. SEE ALSO North American.
T-39 SEE North American.
Thrush Commander SEE Aero Commander
X-30 - NASA project NASP (National Aero-Space Plane) to operate from conventional runways to space and return at speeds more than Mach 5.0.
Rockwell X-31 Proto and tailless version (NASA Dryden)
Rockwell X-31 cockpit (NASA Dryden)
X-31 1990 = 1pClwM; GE F404. Collaborative effort with Messerschmitt-Bolkow-Blohm in Germany in the supersonic, high angle-of-attack X-aircraft program to develop a fighter for flight testing. 1pClwM rg; GE F404; span: 23.10" length: 43'4" load: 4525# v: Mach 1.3; ff:10/11/90 (p: Ken Dyson). POP: 2 for USN as X-31A [164584/164585], the first destroyed in a crash 1/19/95.