Converted from a Grumman Goose amphibian, the K-16B underwent extensive wind tunnel and tethered testing, but was not flown before the project was terminated in 1962.

During the late 1950s, there was extensive interest in the vertical takeoff and landing concept for aircraft, with multiple experimental types ordered to develop the technology for potential service.

The United States Navy contracted with Kaman Aircraft of Bloomfield, Connecticut, to build a testbed based on the company's 'rotorprop' concept for tiltwing aircraft,[1] using a Grumman JRF-5 Goose amphibian and other existing parts to reduce the cost and time necessary.

[2] The fuselage and tail of the Goose were mated to a new tilting wing and engine configuration;[3] the maximum angle of incidence allowed was only 50 degrees; the rotorprop was expected to provide sufficient thrust to allow VTOL operations despite the low angle.

[1] Delivered in late 1959, the K-16B underwent extensive wind tunnel testing, along with some tethered hops, to evaluate the tiltwing configuration's aerodynamic characteristics.