McDonnell Douglas Corporation v. Thiokol Corporation Morton International, Inc.

124 F.3d 1173, 33 U.C.C. Rep. Serv. 2d (West) 768, 97 Daily Journal DAR 11885, 97 Cal. Daily Op. Serv. 7377, 1997 U.S. App. LEXIS 24411, 1997 WL 566764
CourtCourt of Appeals for the Ninth Circuit
DecidedSeptember 15, 1997
Docket96-55239
StatusPublished
Cited by8 cases

This text of 124 F.3d 1173 (McDonnell Douglas Corporation v. Thiokol Corporation Morton International, Inc.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Ninth Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
McDonnell Douglas Corporation v. Thiokol Corporation Morton International, Inc., 124 F.3d 1173, 33 U.C.C. Rep. Serv. 2d (West) 768, 97 Daily Journal DAR 11885, 97 Cal. Daily Op. Serv. 7377, 1997 U.S. App. LEXIS 24411, 1997 WL 566764 (9th Cir. 1997).

Opinion

HUG, Chief Judge.

Thiokol Corporation contracted to provide Star 48 motors to McDonnell Douglas Corporation for inclusion in McDonnell Douglas’ upper-stage Payload Assist Module, which is designed to propel satellites from the Space Shuttle to a geosynchronous orbit 22,000 nautical miles from Earth. In the contract, Thiokol warranted that the motors would be free of defects in material, labor, and manufacture and that the motors would comply with contract drawings and specifications. Following the failure of two satellites to reach their intended orbit, McDonnell Douglas brought this warranty action against Thiokol. The district court entered judgment against McDonnell Douglas after an eleven-day bench trial. We must decide whether Thiokol breached its warranties. We have jurisdiction, 28 U.S.C. § 1291, and we affirm.

Background

In 1976, McDonnell Douglas Corporation (“McDonnell Douglas”) entered a contract with the National Aeronautics and Space Administration (“NASA”) to develop and market an upper-stage Payload Assist Module (“PAM”). The PAM propels satellites from the Space Shuttle to a geosynchronous orbit some 22,000 nautical miles from Earth. It consists of several components, including: (1) a cradle that links the satellite to the Space Shuttle; (2) a mechanism that deploys the satellite from the Shuttle’s cargo bay; (3) an upper-stage motor to move the satellite from the Shuttle’s 160 mile parking orbit into a transfer orbit; and (4) a smaller motor to take the satellite from the apogee of the transfer orbit to its intended orbit. In 1976 there were no upper-stage motors in production that suited McDonnell Douglas’ needs. To obtain such a motor, McDonnell Douglas completed Specification Control Drawing 1B98497 (the “Specification Control Drawing”) on August 18, 1976, which conceptualized a motor that would meet its needs.

In response to the Specification Control Drawing, Thiokol Corporation (“Thiokol”) developed a prehminary design for an upper-stage motor. Thiokol’s prehminary design incorporated a carbon-carbon exit cone, rather than the more common earbon-phenohc exit cone. The use of the hghter carbon-carbon exit cone was necessary in order to comply with the weight limitations set forth in the Specification Control Drawing. Thiok-ol sent its prehminary design to McDonnell Douglas for its review. Because of the “young maturity” of carbon-carbon technology, Thiokol also sent a separate prehminary design of the motor’s nozzle assembly, which indicated that Thiokol planned to use a carbon-carbon cone.

In 1978, Thiokol and McDonnell Douglas entered a contract for the development and qualification of an upper-stage motor. The motor became known as the Star 48 motor. The development and qualification contract was labeled the 7011 contract. This contract established a rigorous series of development and qualification tests that Thiokol’s proposed design had to meet before Thiokol was allowed to begin production.

Before Thiokol could continue with development of the motor under the contract, it had to obtain McDonnell Douglas’ approval of the design. The development phase thus called for a prehminary design review in which McDonnell Douglas and Thiokol engineers jointly reviewed the design of the Star *1175 48 motor. McDonnell Douglas gave Thiokol its approval following the preliminary design review. The approval extended to the carbon-carbon exit cone.

After receiving McDonnell Douglas’ approval, Thiokol conducted five engine test-firings, all of which were witnessed by McDonnell Douglas engineers. McDonnell Douglas engineers were allowed to inspect the motors following the firings and received reports analyzing the results of the tests.

After a second design review, which focused on whether the motor design complied with the requirements of the Specification Control Drawing, McDonnell Douglas again gave Thiokol its approval. Six more motors were test-fired and a qualification program review was held. The purpose of this review was to obtain McDonnell Douglas’ approval of the motor, which was necessary to allow Thiokol to move into the production phase. McDonnell Douglas gave its approval, concluding that the motor met all of the performance and technical requirements of the Specification Control Drawing.

Following qualification of the motor, but before the parties agreed to a production contract, Thiokol test-fired another motor. This test resulted in a motor failure, and an investigation ensued. Although the cause of the failure was not determined with certainty, McDonnell Douglas issued a statement indicating that the most probable cause was a low density/low quality cone. The failure occurred even though the motor met all of the contract’s specification and acceptance requirements.

NASA and the United States Air Force conducted and independent investigation of the test failure. Significantly, this investigation concluded, “The state of knowledge about the material properties of earbon/car-bon involute exit cones is such that a meaningful margin of safety cannot be established for the Star 48 exit cone.” The NASA/Air Force investigation recommended that McDonnell Douglas expand its testing procedures to detect density variations in cones that otherwise met technical and acceptance standards. McDonnell Douglas thus knew that a test firing resulted in a failure, that NASA and the Air Force believed a meaningful margin of safety could not be established, and that its acceptance testing could not detect all density variations. Despite its knowledge, McDonnell Douglas did not adopt the NASA/Air Force recommendations.

McDonnell Douglas and Thiokol entered into a production contract (the “7047 contract”) in 1981. The contract required Thiokol to “maintain the system of producing hardware as established under [the 7011 contract].” The contract also incorporated Article 18 of McDonnell Douglas’ Terms and Conditions Guide. That article provides:

Seller warrants the articles delivered hereunder to be free from defects in labor, material and manufacture, and to be in compliance with any drawings or specifications incorporated or referenced herein ____ All warranties shall run to
[McDonnell Douglas], its successors and assigns, and to its customers and the users of its products.

On February 3, 1984, the Space Shuttle Challenger used the PAM system to deploy WESTAR-VI, a private communications satellite. The WESTAR-VI satellite failed to reach its transfer orbit. An interply density variation, which is an area of reduced density between the layers of carbonized cloth that comprise the carbon-carbon exit cone, caused the Star 48 motor to fail. Three days later, the Challenger deployed the Palapa B-2 satellite, which also failed to reach its transfer orbit because of a motor failure caused by an interply density variation.

On February 7, McDonnell Douglas convened a Failure Investigation Committee to investigate the WESTAR-VI and Palapa B-2 failures (collectively the “failures”).

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124 F.3d 1173, 33 U.C.C. Rep. Serv. 2d (West) 768, 97 Daily Journal DAR 11885, 97 Cal. Daily Op. Serv. 7377, 1997 U.S. App. LEXIS 24411, 1997 WL 566764, Counsel Stack Legal Research, https://law.counselstack.com/opinion/mcdonnell-douglas-corporation-v-thiokol-corporation-morton-international-ca9-1997.