16 September 1999

NASA 008, known as “Balls 8,” a modified Boeing RB-52B-10-BO Stratofortress, serial number 52-008, with NASA 824, a Lockheed TF-104G Starfighter, N824NA. The DAST 1 drone is under the bomber’s right wing. (NASA)

16 September 1999: 44 years, 3 months and 6 days after its very first flight, NASA’s airborne launch aircraft, or “mothership,” Balls 8, completed its 1,000th flight.

Balls 8, so-called because of the double zeros in it U.S. Air Force serial number, 52-008, is a Boeing NB-52, modified as a drop ship from its original configuration as an RB-52B-10-BO Stratofortress reconnaissance bomber assigned to the Strategic Air Command. It made its first flight 11 June 1955 and was reassigned from SAC to Edwards Air Force Base to support NASA flight testing operations, 8 June 1959. Balls 8 served NASA until 17 December 2004, when it was replaced by a newer NB-52H Stratofortress.

52-008 was altered at the North American Aviation facility at Air Force Plant 42, Palmdale, California. A pylon was mounted under the bomber’s right wing. A large notch was cut into the trailing edge of the inboard flap for the X-15’s vertical fin. A 1,500 gallon (5,678 liter) liquid oxygen tank was installed in the bomb bay. A station for a launch operator was installed on the upper deck of the B-52 at the former electronic countermeasures position. A series of control panels allowed the panel operator to monitor the X-15’s systems, provide electrical power, and to keep the rocketplane’s liquid oxygen tank full as the LOX boiled off during the climb to launch altitude. The operator could see the X-15 through a plexiglas dome, and there were two television monitors.

The NB-52B was used during the X-15 Program and carried the three hypersonic research aircraft aloft on 159 of their 199 flights. (NB-52A 52-003, The High and Mighty One, made the other 40 launches.) It has also been used to carry the X-24 and HiMat lifting body research aircraft and to launch Pegasus research rockets.

At the time of its retirement, Balls 8 was the oldest B-52 in service, and also the lowest time B-52. It is on display near the north gate at Edwards Air Force Base.

Balls 8, Boeing NB-52B Stratofortress 52-008, as seen from a KC-135A Stratotanker. (NASA)
Balls 8, NASA’s Boeing NB-52B Stratofortress 52-008 “mothership”, as seen from a KC-135A Stratotanker. (NASA)

Of the 744 B-52 Stratofortresses built by Boeing, 50 were B-52Bs and 27 of these were RB-52B reconnaissance bombers.

The airplane was 156 feet, 6.9 inches (47.724 meters) long with a wingspan of 185 feet, 0 inches (56.388 meters) and overall height of 48 feet, 3.6 inches (14.722 meters). The wings were mounted high on the fuselage (“shoulder-mounted”) to provide clearance for the engines which were suspended on pylons. The wings’ leading edges were swept 35°. The bomber’s empty weight was 164,081 pounds (74,226 kilograms), with a combat weight of 272,000 pounds (123,377 kilograms) and a maximum takeoff weight of 420,000 pounds (190,509 kilograms).

Early production B-52Bs were powered by eight Pratt & Whitney J57-P-1W turbojet engines, while later aircraft were equipped with J57-P-19W and J57-P-29W or WA turbojets. The engines were grouped in two-engine pods on four under-wing pylons. The J57 was a two-spool, axial-flow engine with a 16-stage compressor section (9 low- and 7-high-pressure stages) and a 3-stage turbine section (1 high- and 2 low-pressure stages). These engines were rated at 10,500 pounds of thrust (46.71 kilonewtons), each, or 12,100 pounds (53.82 kilonewtons) with water injection.

The B-52B/RB-52B had a cruise speed of 523 miles per hour (842 kilometers per hour). The maximum speed varied with altitude: 630 miles per hour (1,014 kilometers per hour) at 19,800 feet (6,035 meters), 598 miles per hour (962 kilometers per hour) at 35,000 feet (10,668 meters) and 571 miles per hour (919 kilometers per hour) at 45,750 feet (13,945 meters). The service ceiling at combat weight was 47,300 feet (14,417 meters).

Maximum ferry range was 7,343 miles (11,817 kilometers). With a 10,000 pound (4,536 kilogram) bomb load, the B-52B had a combat radius of 3,590 miles (5,778 kilometers). With inflight refueling, the range was essentially world-wide.

This "score board" painted on the side of Balls 8 shows many of the missions that it flew as a "mothership" for NASA. (NASA)
This “score board” painted on the side of Balls 8 shows many of the missions that it flew as a “mothership” for NASA. (NASA)

Defensive armament consisted of four Browning Aircraft Machine Guns, Caliber .50, AN-M3, mounted in a tail turret with 600 rounds of ammunition per gun. These guns had a combined rate of fire in excess of 4,000 rounds per minute. (Eighteen RB-52Bs were equipped with two M24A1 20 mm autocannon in the tail turret in place of the standard four .50-caliber machine guns.)

The B-52B’s maximum bomb load was 43,000 pounds (19,505 kilograms). It could carry a 15-megaton Mark 17 thermonuclear bomb, or two Mark 15s, each with a maximum yield of 3.8 megatons.

Balls 8 lands on a runway marked on Rogers Dry Lake at Edwards Air Force Base, California. The drogue parachute helps to slow the airplane. (NASA)
Balls 8 lands on a runway marked on Rogers Dry Lake at Edwards Air Force Base, California. The drogue parachute helps to slow the airplane. (NASA)

© 2017, Bryan R. Swopes

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11 thoughts on “16 September 1999

  1. Enjoyed the “facts” presented for this aircraft…great article. Thanks! I was a fan of the movie “X15”; as a kid I watched it at least 5 times…wonder if Balls 008 was in it?

    1. Thank you, Bryan. Though I am certainly aware of the movie, I don’t think that I ever actually watched it, so I don’t know. But probably Balls Eight would have been seen in it.

  2. Howdy Bryan. Do you know if they did anything special to balance the mothership when carrying a wing mounted craft such as the X-15? Asymmetrical fuel load or something, or was the load within balance limits? Thanks.

    1. Steve, that is an EXCELLENT question. I don’t know, but let me do some research and I’ll get back to you. Thanks for giving me something to think about. —Bryan

  3. To answer Steve Johnson’s question:
    To compensate for the weight and drag of the X-15, trim settings were adjusted to left wing down and slight right rudder for take-off. The wings were leveled when the ailerons became effective as the airspeed increased.

  4. Oh, I failed to mention this as well:
    When the X-15 was launched, the right wing of the NB-52B was suddenly relieved of about 35,000 pounds of weight. The weight of the X-15 was offset forward and to the right of the center of gravity of the Stratofortress, so launching the X-15 produced a roll to the left and a pitch up. The application of half aileron to the right and forty pounds of push force on the stick would counteract the attitude change.

  5. Thanks to all.
    Thanks Bryan for providing this forum about aviation.
    Thank you Jim for sharing your insight on the topic, as well to other commenters who share their personal experiences and aerospace knowledge.
    This is such a great site.
    Thank you again.

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