United Aircraft Corporation v. Paul Hardeman, Inc.

204 A.2d 396, 58 Del. 66, 8 Storey 66, 1964 Del. Super. LEXIS 92
CourtSuperior Court of Delaware
DecidedOctober 22, 1964
Docket199
StatusPublished
Cited by4 cases

This text of 204 A.2d 396 (United Aircraft Corporation v. Paul Hardeman, Inc.) is published on Counsel Stack Legal Research, covering Superior Court of Delaware primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
United Aircraft Corporation v. Paul Hardeman, Inc., 204 A.2d 396, 58 Del. 66, 8 Storey 66, 1964 Del. Super. LEXIS 92 (Del. Ct. App. 1964).

Opinion

DUFFY, President Judge.

This is an action by United Aircraft Corporation (“United Aircraft”) against Paul Hardeman, Inc. (“Hardeman”) for moneys owed as a result of work performed by the Hamilton Standard Division of United Aircraft (“Hamilton Standard”) for Hardeman. Hardeman counterclaimed for losses caused by Hamilton Standard.

Hamilton Standard, an operating division of United Aircraft, has long been active in the aircraft industry and, in recent years, has directed resources toward meeting the United States Government’s requirements in the missile programs. Hardeman is a large engineering and construction company engaged in various projects around the world.

In the spring of 1961, Hamilton Standard’s personnel, including those servicing the aircraft industry in southern California, were aware that the Air Force planned to construct silos for the emplacement of *68 operational Titan II missiles. The Titan II is an intercontinental ballistic missile employed in the national defense of the United States.

The Titan II program included a single prime contract for manufacturing, delivering, installing and validating 57 fixed Propellant Transfer Systems (“PTS”) and 9 (later increased to 10) units of mobile propellant transfer equipment at 4 general sites in California, Arizona, Kansas and Arkansas. That contract included 9 (also increased to 10) waste propellant disposal trailers for. use with the fixed and mobile PTS facilities.

A Propellant Transfer System is the device or means for handling, loading and unloading the propellant used in the Titan II. The propellant consists of fuel and an oxidizer. 1 At the 57 launch facilities, the Propellant Transfer Systems were to be installed in silos, which are large reinforced concrete underground chambers. These were to be constructed under the terms of contracts other than the contract for the Propellant Transfer Systems. The mobile PTS units, including the waste propellant disposal equipment, were to be mounted on trailers and used in conjunction with the fixed propellant transfer facilities for transferring propellant to and from the missile propellant tanks and for disposing of waste propellant.

If a missile were drained without firing (and it was expected that this would be done with some regularity), then the propellant would have to be burned. The waste propellant disposal trailers called for under the PTS prime contract were mobile pieces of equipment designed to burn waste propellant. That propellant consists of the fuel and oxidizer vapors. Burning is necessary so that the highly toxic liquid waste and fumes are reduced to a condition not injurious to human life.

The subcontract to manufacture the waste propellant disposal trailers is the matter involved in this action.

*69 Hamilton Standard had had prior experience with the disposal of waste gosses in the research place of the Titan II program. Specifically, it had completed a test program for the Martin Company to determine the feasibility of destroying aerozine and nitrogen tetroxide vapors by burning.

Following a practice common in the aerospace industry, Hamilton Standard set about informing the potential prime contractors of its capabilities. One of these was Hardeman, which had been involved in various phases of missile base construction projects. The Air Force had invited Hardeman and seven others to submit project proposals for the prime contract. Following up its various prior sales efforts, Hamilton Standard submitted to Hardeman on May 23, 1961 a management proposal in which its prior experience and know-how were emphasized. This proposal was essentially a sales promotion piece designed to secure a contract for all mobile equipment called for by the prime contract. Similar proposals were sent by Hamilton Standard to the other potential prime contractors, and all were followed up by its sales and technical personnel.

On July 1, 1961 the Air Force announced that it had awarded the Titan II prime contract for the propellant transfer systems to Hardeman. Thereafter Hardeman intensified its negotiations v/ith various potential subcontractors, including Hamilton Standard. These culminated in a three-day meeting with Hamilton Standard at Hardeman’s offices in California attended by technical and management people from both sides. Near the end of the meeting, on August 17, Hamilton Standard hand-delivered a letter to Hardeman reading as follows:

“Submitted herewith is our revised quotation for the subject equipment to include the additional requirements as discussed in our meeting of August 16 and those as set forth in your letter dated July 31,1961.

“For clarification, we wish to restate that the equipment being offered herewith is in conformance with un-numbered and un-dated *70 specification entitled ‘Waste Propellant Disposal Trailer’ identified as Section 9 as amended by attachment A. It should be noted that the proposed hardware completely meets the specified performance but deviates from some of the detailed requirements of the aforementioned unnumbered specification. We are prepared to review attachment A with your people at your earliest convenience in order to resolve any questions you may have.

“Regarding the requirements of your July 31 letter, attachment B summarizes our comments to the ‘Special Requirements’ section contained therein. Thesé requirements are acceptable with the exceptions as noted in attachment B. The requirements of your July 31 letter dealing with drawings per MIL — D—70327 are acceptable but acceptance of AFBM Exhibit 60 — 3A and WDT Exhibits 57 — 17 must remain open until such time these documents are available for our review.

“Delivery of ten each of the subject units is noted as follows based on an August 18,1961 contract go ahead:

1 unit by December 31,1961

1 unit by January 28,1962

1 unit by February 25,1962

1 unit by March 25,1962

1 unit per month thereafter to completion.

“The above schedule reflects on dock dates at the Hamilton Standard plant, Windsor Locks, Connecticut.

“Our cost quotation for the design, fabrication, testing and delivery of ten each of the subject units to the above schedule is $385,250. This quotation includes a one percent (1%) rental factor for Government-Owned Facilities under Navy Facilities Contract No. A-5929. Rent free use statement in any resulting contract will decrease the contract price by one percent (1%).

“Our cost quotation for the MIL — D—70327 drawing *71 requirement of your July 31 letter is $18,000 while the cost of the operation and maintenance data per Paragraph 5 of the Special Requirements attachment of your July 31 letter is $6,500.

“Hamilton Standard will per Section 7 of Special Requirements furnish representatives at sites or where ever needed to supervise and train personnel in the proper operation and maintenance during the field checkout and testing of the propellant waste disposal units and the completed propellant transfer system. However, this service is not considered part of our present offering.

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204 A.2d 396, 58 Del. 66, 8 Storey 66, 1964 Del. Super. LEXIS 92, Counsel Stack Legal Research, https://law.counselstack.com/opinion/united-aircraft-corporation-v-paul-hardeman-inc-delsuperct-1964.