ASSET (spacecraft)

ASSET
Preserved ASSET vehicle at USAF Museum, Dayton, Ohio
Role	Spaceplane research — never flew beyond Earth's atmosphere
Manufacturer	McDonnell Aircraft
First flight	September 18, 1963
Status	Museum piece
Primary user	United States Air Force
Number built	6
Developed from	Boeing X-20 Dyna-Soar
Variants	Winged Gemini

ASSET pre-launch checkout.

ASSET-Thor combination on Pad 17B.

ASSET, or Aerothermodynamic Elastic Structural Systems Environmental Tests was an experimental US space project involving the testing of an uncrewed sub-scale reentry vehicle.

Development and Testing

Begun in 1960, ASSET was originally designed to verify the superalloy heat shield of the X-20 Dyna-Soar prior to full-scale crewed flights. The vehicle's biconic shape and low delta wing were intended to represent Dyna-Soar's forward nose section, where the aerodynamic heating would be the most intense; in excess of an estimated 2200 °C (4,000 °F) at the nose cap. Following the X-20 program's cancellation in December 1963, completed ASSET vehicles were used in reentry heating and structural investigations with hopes that data gathered would be useful for the development of future space vehicles, such as the Space Shuttle.

Built by McDonnell, each vehicle was launched on a suborbital trajectory from Cape Canaveral's Pad 17B at speeds of up to 6,000 m/s before making a water landing in the South Atlantic near Ascension Island. Originally, a Scout launch vehicle had been planned for the tests, but this was changed after a large surplus of Thor and Thor-Delta missiles (returned from deployment in the United Kingdom) became available.

Of the six vehicles built, only one was successfully recovered and is currently on display at the National Museum of the United States Air Force in Dayton, Ohio.

Flights

Mission	Launch Date	Apogee	Max. Speed	Result	Disposition
ASSET 1	September 18, 1963	62 km	4,906 m/s	Survived reentry; flotation equipment malfunctioned, preventing planned recovery.	Sunk in Atlantic.
ASSET 2	March 24, 1964	55 km		Launch vehicle upper stage malfunction; vehicle self-destruct mechanism activated post-separation. Mission failed.	Destroyed.
ASSET 3	July 22, 1964	71 km	5,500 m/s	Survived reentry; all mission goals met.	Recovered 12 hours after launch. Preserved.
ASSET 4	October 28, 1964	50 km	4,000 m/s	Survived reentry; all mission goals met; recovery not planned.	Sunk in Atlantic.
ASSET 5	December 9, 1964	53 km	4,000 m/s	Survived reentry; all mission goals met; recovery not planned.	Sunk in Atlantic.
ASSET 6	February 23, 1965	70 km	6,000 m/s	Survived reentry; flotation equipment malfunctioned, preventing planned recovery.	Sunk in Atlantic.

Specifications

ASSET 3-view

General characteristics

• Crew: None

Performance

• Hypersonic L/D Ratio: 1:1

Related content

Comparable Aircraft

• Molniya BOR-4
• Martin X-23 PRIME

Winged Gemini

In the mid-1960s, McDonnell proposed a variant of the Gemini capsule which retained the original spacecraft's internal subsystems and crew compartment, but dispensed with the tail-first ballistic reentry, parachute recovery and water landing.

Instead, the vehicle would be heavily modified externally into an ASSET-like lifting-reentry configuration. Post-reentry, a pair of stowed swing-wings would be deployed, giving the spacecraft sufficient L/D to make a piloted glide landing on a concrete runway using a skid-type landing gear (reinstated from the planned, but cancelled paraglider landing system), much like the Space Shuttle.

According to Mark Wade's Encyclopedia Astronautica, the intent seems to have been to field a crewed military spaceplane at a minimal cost following the cancellation of the Dyna-Soar program.