UB Paderborn / Katalog / Suche / in CDI

Specific transportation costs to GEO — past, present and future

Acta astronautica, 2003-08, Vol.53 (4), p.797-803

Koelle, D.E.

2003

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The cost-optimal size of future reusable launch vehicles

Acta astronautica, 2000-07, Vol.47 (2), p.205-213

Koelle, D.E

2000

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Space launch systems cost estimation as design tool

Acta astronautica, 1994-10, Vol.34, p.175-181

Koelle, D.E.

1994

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Cost reduction for future communication satellites by a standardized propulsion module (OPM)

Acta astronautica, 1988, Vol.17 (4), p.397-405

1988

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Cost efficiency as design and selection criterion for future launch vehicles

Acta astronautica, 2005-07, Vol.57 (2), p.623-629

Koelle, Dietrich E.

2005

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Sänger II, an advanced launcher system for Europe

Acta astronautica, 1989, Vol.19 (1), p.63-72

1989

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The single-stage reusable ballistic launcher concept for economic cargo transportation

Acta astronautica, 1987-01, Vol.16, p.125-130

1987

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Geostationäre Nachrichtensatelliten

Kommunikation über Satelliten / Communication via Satellites, p.19-33

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A cost-engineered launch vehicle for space tourism

Acta astronautica, 1999, Vol.44 (7), p.649-656

Koelle, Dr.-Ing.Dietrich E.

1999

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Economics of small fully reusable launch systems (SSTO vs. TSTO)

Acta astronautica, 1997, Vol.40 (2), p.535-544

Koelle, Dietrich E.

1997

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Reusable Launch Vehicles (RLVs) and Cost Engineering Principles

The Space Transportation Market: Evolution or Revolution?, p.157-166

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Cost analysis for single-stage (SSTO) reusable ballistic launch vehicles

Acta astronautica, 1993-07, Vol.30, p.415-421

Koelle, Dietrich E.

1993

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The single-stage resuable ballistic launcher concept for economic cargo transportation

Acta astronautica, 1987, Vol.16, p.125-130

1987

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Launch cost analyses for reusable space transportation systems (Sänger II)

Acta astronautica, 1989, Vol.19 (2), p.191-197

Koelle, Dietrich E.

1989

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The transcost-model for launch vehicle cost estimation and its application to future systems analysis

Acta astronautica, 1984-01, Vol.11 (12), p.803-817

Koelle, Dietrich E.

1984

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Launch vehicle evolution - from multistage expendables to single-stage reusables

Acta astronautica, 1986, Vol.14, p.159-166

Koelle, Dietrich E.

1986

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Orbital transfer systems for lunar missions

Acta astronautica, 1992-08, Vol.28, p.85-89

1992

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Cost reduction trends in space communications by larger satellites/platforms

Acta astronautica, 1984-01, Vol.11 (12), p.785-794

Koelle, Dietrich E.

1984

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On the optimum cruise speed of a hypersonic aircraft

IEEE aerospace and electronic systems magazine, 1989-05, Vol.4 (5), p.13-16

Koelle, D.E.

1989

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The impact of launch vehicle type and size on development cost

Acta astronautica, 1981-01, Vol.8 (11), p.1195-1205

Koelle, Dietrich E.

1981

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Advanced Technology for Direct TV-Broadcasting Satellites

Journal of spacecraft and rockets, 1980-03, Vol.17 (2), p.79-85

Koelle, Dietrich E

1980

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Future low-cost space transportation system analysis

Acta astronautica, 1979-01, Vol.6 (12), p.1635-1667

1979

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Bücherschau

Forschung im Ingenieurwesen, 1966-07, Vol.32 (4), p.129-132

1966

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Bücherschau

Forschung im Ingenieurwesen, 1964-05, Vol.30 (3), p.93-96

1964

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Quantitative nanoscale vortex imaging using a cryogenic quantum magnetometer

Nature nanotechnology, 2016-08, Vol.11 (8), p.677-681

2016

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Specific transportation costs to GEO — past, present and future

The cost-optimal size of future reusable launch vehicles

Space launch systems cost estimation as design tool

Cost reduction for future communication satellites by a standardized propulsion module (OPM)

Cost efficiency as design and selection criterion for future launch vehicles

Sänger II, an advanced launcher system for Europe

The single-stage reusable ballistic launcher concept for economic cargo transportation

Geostationäre Nachrichtensatelliten

A cost-engineered launch vehicle for space tourism

Economics of small fully reusable launch systems (SSTO vs. TSTO)

Reusable Launch Vehicles (RLVs) and Cost Engineering Principles

Cost analysis for single-stage (SSTO) reusable ballistic launch vehicles

The single-stage resuable ballistic launcher concept for economic cargo transportation

Launch cost analyses for reusable space transportation systems (Sänger II)

The transcost-model for launch vehicle cost estimation and its application to future systems analysis

Launch vehicle evolution - from multistage expendables to single-stage reusables

Orbital transfer systems for lunar missions

Cost reduction trends in space communications by larger satellites/platforms

On the optimum cruise speed of a hypersonic aircraft

The impact of launch vehicle type and size on development cost

Advanced Technology for Direct TV-Broadcasting Satellites

Future low-cost space transportation system analysis

Bücherschau

Bücherschau

Quantitative nanoscale vortex imaging using a cryogenic quantum magnetometer

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