RESUSCITATION AND TREATMENT OF THE INJURED.

Abstract

The first section of the report has to do with the evaluation of various regimens of replacement therapy in hemorrhagic shock. This was done in dogs by producing a standard shock model from bleeding. The animal is resuscitated with a variety of replacement solutions and then a second shock is given them 24 hours later. It is the purpose of this study to determine the animal's ability to withstand a second shock after being treated initially with a variety of replacement methods. Another aspect has to do with pulmonary manifestations of trauma. Experiments were designed to test the hypothesis that following burn injury and postperfusion lung, increased transudation of plasma from the capillary space to the interstitial fluid space and subsequently to the bronchoalveolar space resulted in destruction of pulmonary surfactant with secondary development of congestive atelectasis and respiratory distress syndrome. In bioengineering several developments occurred including an expansion of the use of the X-grid and improvement in low flow hemodialysis with the SCIRT Mark III pump. A new device, the self powered infusion pump, is in the final design stage. It is hoped that this will provide a way of infusing fluids in battlefield and other situations without the use of gravity. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1969
Accession Number
AD0698479

Entities

People

  • Curtis P. Artz

Organizations

  • Medical University of South Carolina

Tags

DTIC Thesaurus Topics

  • Anatomy
  • Artificial Organs
  • Battlefields
  • Bioengineering
  • Biological Sciences
  • Blood
  • Burns
  • Hemorrhagic Shock
  • Infusions
  • Lung Diseases
  • Microvessels
  • Respiratory System Agents
  • Resuscitation
  • Standards
  • Surface Active Substances
  • Test And Evaluation

Fields of Study

  • Medicine

Readers

  • Cardiovascular Physiology
  • Systems Analysis and Design

Technology Areas

  • Biotechnology
  • Space
  • Space - Hall-Effect Thruster