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METU · The 1960s

ORDOT

A guided rocket research and development project carried out at METU in the 1960s. This page was prepared to tell the story of that team's work, with its sources.

ORDOTIllustrative drawing. ORDOT's dimensions are not given in the sources, so proportions may differ from the real rocket.
The Story

One department, one team, one rocket.

“Even though very valuable years were lost, things are finally happening in Türkiye.”

Prof. Nuri Saryal, from his ORDOT memoirs

In the early 1960s Türkiye bought its wire-guided anti-tank rockets from abroad. Prof. Nuri Saryal, who joined the METU Department of Mechanical Engineering in 1962, believed this technology could be researched at the university and brought together a team of faculty members, assistants and technicians from several departments.

The project ran for about three years. The team prepared its own solid propellant, fired the motor again and again in its own test room, developed proportional guidance electronics and designed a parachute head to recover the test rocket. The flight tests held on METU land in 1969 were widely reported in the press.

ORDOT remained a research and development project and never went into production. Even so, it left behind methods, trained people and a memory on campus.

~3years
Length of the project
77
The first motor test without an explosion came at about this attempt
2km
Planned length of the command wire
1969
Year of the flight tests
Video

ORDOT, as told by METU.

The episode of METU's “Bilim Her Yerde” series devoted to the ORDOT project (in Turkish).

Bilim Her Yerde | ORDOT ProjesiVideo: ODTÜ-METU YouTube channel (in Turkish)
Design

What was inside the rocket?

Tap the numbers to read how each part was designed. The information is based on the memoirs of Prof. Nuri Saryal.

ORDOT123456Illustrative drawing. ORDOT's dimensions are not given in the sources, so proportions may differ from the real rocket.
01

Parachute head

Designed so that the test rocket could be recovered. An acceleration switch, adjustable between 5 and 20 seconds, released the parachute. The head worked in both catapult tests carried out above an abandoned quarry.

Suha Selamoğlu, Vedat Arpacı
From the design desk
  • Composite partsMade from glass fibre and polyester. The idea came from technician Esat Aşkun; the polyester was sourced from İzmir.
  • Trajectory calculationThe flight path was calculated with a program written for a punched-card IBM computer (Levent Kayalar).
  • Equations of motionOrhan Kural worked on the equations describing the rocket's behaviour in flight.
Timeline

ORDOT, from 1962 to 1970.

28 June 1962

Nuri Saryal at METU

Prof. Nuri Saryal joined the METU Department of Mechanical Engineering.

  1. 28 June 1962Nuri Saryal at METU

    Prof. Nuri Saryal joined the METU Department of Mechanical Engineering.

  2. 1964 – 1965Building and laboratories

    The Mechanical Engineering building and its laboratories were completed, laying the ground for experimental work.

  3. Second half of the 1960sThe project begins

    Work that would last about three years began. An agreement was made with the Air Force Command, and the motor test room was built next to the NATO project building of Electrical Engineering.

  4. About the 77th attemptFirst motor test without an explosion

    After dozens of attempts the motor burned without exploding for the first time. Step by step, the team had solved its propellant casting and burning-surface problems.

  5. 31 May 1969Decision for the first flight test

    According to Saryal's account, on a sunny Saturday the rocket left the ramp cleanly, climbed in the calculated direction and went out of sight. The test was filmed with a 16 mm Bolex camera.

  6. 22 – 30 June 1969ORDOT in the press

    The daily Milliyet reported the project on its front page on 22 June. The second successful test on 28 June appeared in the paper on 30 June.

  7. 1 April 1970End of an era

    Saryal left for Munich on a Humboldt fellowship. The project remained at the research and development stage.

  8. AfterwardsTraces

    In later years the Guided Vehicles Test and Measurement Centre (GATÖM) was founded and was later succeeded by SAGE. Ömer Anlağan of the ORDOT team went on to serve as director of SAGE.

ORDOT on Campus

Where were the tests held?

01

Motor test room

Built next to the NATO project building of Electrical Engineering. The motor was fired here again and again on the thrust measuring rig.

02

The quarry

The parachute head was tested by launching it with a catapult above an abandoned quarry. Both tests were successful.

03

Launch area

The first flight test took place on METU land, in an empty area used for burning refuse.

Support

Who supported the project?

  • METU Rectorate40,000 TL

    Initial funding provided under Rector Kemal Kurdaş.

  • Air Force Command140,000 TL

    Agreement arranged through Colonel Cemal Özalp; support was also given on aerodynamics.

  • Motor test room55,000 TL

    Built under Vice Rector Orhan Alsaç.

  • TPAOMaterials

    Asphalt for the propellant was supplied through Korkut Özal.

  • Hacettepe University RadiologyX-ray

    With the support of Abdullah Kenanoğlu, the propellant grains were checked by X-ray.

The Team

The people behind ORDOT.

The roles are based on the memoirs of Prof. Nuri Saryal. We would not want to leave anyone's work out: if you have a photograph, a document or a correction to share, please write to us.

Prof. Nuri Saryal

Project lead · Mechanical Engineering

Born in Baku in 1929. He graduated from Robert College in mechanical engineering in 1952, took his master's degree at Purdue University and his doctorate at the Technical University of Berlin (1956). He joined METU in 1962, chaired the department in 1963–1965 and served as Rector of METU in 1977–1979. He started and led ORDOT. He passed away in 2020.

Prof. Suha Selamoğlu

Parachute head, propellant moulds, design and manufacture · Mechanical Engineering

Born in Ankara in 1929. He graduated from Istanbul Technical University in 1952 and completed his doctorate at Brown University in 1964. He joined METU Mechanical Engineering in 1966 and worked on fluid mechanics and heat transfer. He passed away in 2022.

Orhan Kural

Equations of motion · Mechanical Engineering

A member of the core team; he worked on the equations describing the rocket's behaviour in flight.

Ömer Anlağan

Research · Mechanical Engineering

Nuri Saryal's thesis student. He later served as director of SAGE.

Ertuğrul Onat

Propellant chemistry · Chemistry

Took on the preparation of the perchloric acid needed for the oxidiser.

Canan Toker

Guidance electronics · Electrical Engineering

Developed the electronics of the proportional guidance.

Mustafa Doruk

Nozzle · Metallurgical Engineering

Worked on the chrome-plated nozzle.

Vedat Arpacı

Parachute head · Visiting faculty

Worked on the parachute head while on sabbatical from the University of Michigan at METU Mechanical Engineering.

Alp Esin

Thrust measurement

Built the rig that measured the motor's thrust.

İlhan Onur

Command wire

Built the machine that wound the command wire.

Levent Kayalar

Trajectory program

Wrote the computer program that calculated the flight trajectory.

Nihat Çokyücel

Workshop manager

Ran the manufacture of the rocket casing.

Esat Aşkun

Technician

Came up with the idea of using composite material.

Metin Özbek

Technician

Made the trips to İzmir to obtain materials.

Orhan Yeşin

Assistant

Worked on the project as Nuri Saryal's assistant.

Today

The same campus, a new generation.

Galaxy Roket does not claim to be the continuation or the heir of ORDOT. We are students designing rockets on the same campus, and we believe it is worth knowing the work of a team that wrestled with similar questions half a century before us.

The story of a team that fired its motor dozens of times, rebuilt it, and made its own mould, press and measuring rig is a good reminder for every day we spend in the workshop.

“Even though very valuable years were lost, things are finally happening in Türkiye.”

Prof. Nuri Saryal, from his ORDOT memoirs
Sources

What is this page based on?

The information here was compiled from the open sources below. ORDOT's length, diameter, weight and the altitude it reached are not given in these sources, so they are not given on this page either.