USAAVLABS technical reports. 64-68M. Heavy-lift tip turbojet rotor system: v. 13, Preliminary model specification for Continental model 357-1 engine.
Publication Title:
Heavy-lift tip turbojet rotor system: v. 13, Preliminary model specification for Continental model 357-1 engine.
Display Title:
USAAVLABS technical reports. 64-68M. Heavy-lift tip turbojet rotor system: v. 13, Preliminary model specification for Continental model 357-1 engine.
Series Title:
USAAVLABS technical reports.
Corporate Agency Authors:
Army Department and Defense Dept.
Sort Author:
Army Department
Author place:
Washington, D.C.
Author zip:
20310
Date:
Oct. 1965
Publish Date ISO Format:
1965-10-01T00:00:00Z
Publication Start:
19651001
Publication End:
19651031
Corporate/Agency Author:
Army Department
Publication month:
3
Publication year:
1965
SuDoc number:
D 117.8/2:(nos.)
Description:
vi+48+[2] p. il. 4°
Notes:
(Task 1M12140D-14412, contract DA 44-177-AMC-25(T).) [Prepared for Hiller Aircraft Company, Inc., by Continental Aviation and Engineering Corporation.] and (Army Aviation Materiel Laboratories, Fort Eustis, Va.)
Notes:
(Army Aviation Materiel Laboratories, Fort Eustis, Va.) Φ For Sale by OTS, Commerce Dept. (Price upon application).
Availability:
Φ For Sale by OTS, Commerce Dept. (Price upon application).