I looked into this and a motor glider must have certain specs to qualify.

IIRC, wing span to gross weight.  However, the sonex page states that
tyhis may not apply to experimental category, and certainly a 27ft
wingspan on a KR1 would fly more like a glider. Especially if equipped
with a full feathering prop for example.

Here it is:

https://www.sonexaircraft.com/aircraft-certification/


Definition of Motorglider or Powered Sailplane

Sonex Aircraft, LLC accepts the formal definition of Powered
Sailplanes for Type Certificated Aircraft from both the United States
and the European Aviation Authorities. While it is not formally
defined that an Aircraft Registered in the Experimental Category must
meet these same criteria, any aircraft which does meet the criteria is
an indisputable "Motorglider" or "Powered Sailplane." The language in
both the U.S. and the European documents are nearly identical and the
portion of the documents which apply to this definition as follows:



United States Department of Transportation, Federal Aviation Administration
Advisory Circular AC 21-17a, dated 10 February 1993

7. ACCEPTABLE CRITERIA.
  b. Additional Criteria for Powered Gliders.
    (1) Powered fixed wing gliders may be type certificated under
Section 21.17(b) if:
      (i) The number of occupants does not exceed two;
      (ii) Maximum weight does not exceed 850 kg (1874 pounds); and
      (iii) The maximum weight to wing span squared (w/b2) does not
exceed 3.0 kg/M2 (0.62 lb./ft.2).
NOTE: These criteria originated from JAR-22.

Joint Aviation Authorities
JAR-22 Amendment 7, dated 1 September 2003

JAR 22.1 Applicability
(a) This JAR-22 prescribes minimum airworthiness standards for the
issue of type certificates, and changes to those certificates, for
sailplanes and powered sailplanes in the utility U and aerobatic A
categories:
  (1)  Sailplanes the maximum weight of which does not exceed 750 kg:
  (2)  Single engine (spark- or compression-ignition) powered
sailplanes the design value W/b2 (weight to span2) of which is not
greater than 3(W[kg], b[m]) and the maximum weight of which does not
exceed 850 kg: and
  (3)  Sailplanes and powered sailplanes the number of occupants of
which does not exceed two.

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