SP-4012 NASA HISTORICAL DATA BOOK: VOLUME III
PROGRAMS AND PROJECTS 1969-1978
 

Table 5-12. HL-10 Lifting Body Characteristics.

 

Shape:

Half-cone body (round top, flat bottom) with blunt nose and three vertical tail fins.

Dimensions (m):

Length:

6.75

Width:

4.59

Height:

3.48

Engine:

XLR-11

Weight (kg):

2400 (with water ballast test tanks full, 4100)

Construction:

Aluminum

Controls:

Thick elevon between each fin and center fin for pitch and roll; split rudder on center fin for yaw and speed brake

First flight:

December 22, 1966

Last flight:

July 17, 1970

Times flown:

37

Test pilots:

Bruce A. Peterson, Jerauld R. Gentry, John A. Manke, William H. Dana, Peter Hoag

Cognizant:

LaRC (design)

NASA center:

FRC (flight testing)

Program manager:

John McTigue, FRC

Contractor:

Northrop Corporation, prime

Remarks:

Also used to simulate Shuttle prototype approach and landing sequence.

Mode of operation:

Released in midair from under the wing of a B-52.


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